Soyuz 2-1A Rocket Body

NORAD ID: 40620
Object: SL-4 R/B
Origin: Russia
Type: Block I Soyuz Upper Stage
Mass: 2,355 Kilograms
Launch: April 28, 2015 – 7:09:50 UTC
Launch Site: 31/6 Baikonur Cosmodrome
Launch Vehicle: Soyuz 2-1A
Ascent Duration: 8 Minutes & 45 Seconds
Payload: Progress M-27M (7,289kg)

 Target Orbit: 193 by 238km, 51.67°
Last Orbit Data: 186 by 257km, 51.65°

Orbital Lifetime: 24 Hours & 23 Minutes (17 Orbits)
Re-Entry Prediction: April 29, 2015 – 7:32 UTC +/-1 Minute
Re-Entry Location: Pacific, 890km west of the Chilean Coast
Picture
Image: Spaceflight101/Google Maps

Falcon 9 Rocket Body

NORAD ID: 40589
Origin: USA
Object: Falcon 9 R/B
Type: Falcon 9 Second Stage
Inclination: 51.6°
Launched: April 14, 2015 - 20:10 UTC
Launch Vehicle: Falcon 9 v1.1 (F9R)
Launch Site: SLC-40 Cape Canaveral Air Force Station
Re-Entry Prediction: April 22, 2015 - 19:00 UTC +/- 1 Minute
Re-Entry Zone: North Africa


Launched the Dragon SpX-6 Mission to the International Space Station
>>>Mission Updates

Re-Entry Zone

Picture
Image: Orbitron

Vostok Rocket Body

NORAD ID: 12072
Origin: Russia
Object: SL-3 R/B
Type: Vostok Rocket Body
Inclination: 81.1°
Launched: November 21, 1980 - 11:53 UTC
Launch Vehicle: Vostok 8A92M
Launch Site: Plesetsk Cosmodrome, Russia
Re-Entry Prediction: April 18, 2015 - 14:19 UTC +/- 1 Minute
Re-Entry Zone: Murmanskaya, Russia


Launched the Kosmos-1222 Satellite

Re-Entry Zone

Picture
Image: Orbitron

TechEdSat-4

NORAD ID: 40455
Launched: Aboard Cygnus Orb-2 Spacecraft
Released from ISS: March 4, 2015 - 01:20 UTC
Origin: USA
Type: 3U CubeSat
Mass: 3 Kilograms
Inclination: 51.6°

Re-Entry Prediction: April 3, 2015 - 09:01 UTC +/- 51 Minutes
Re-Entry Zone: Unknown
TechEdSat-4 flew an Exo-Brake to orbit that was deployed once the satellite was released to demonstrate a Passive De-Orbit System for satellites. The Exo Brake is a deployable device for use in free molecular flow regimes in an exo-atmosphere environment. The device is a tension based structure that has a number of advantages over other designs such as high stability and the possibility of drag modulating to provide targeting capability.
As part of its demonstration in orbit, TechEdSat's Exo-Brake would be deployed to begin a 10-day de-orbit experiment during which the GPS unit of the satellite provides position data that is coupled with Earth-based tracking data to model the exo-atmospheric descent of the satellite. TechEdSat was to have a high ballistic coefficient of 5kg/m² leading to a rapid orbital decay.

Re-Entry Orbit

Picture
Image: Orbitron

ORS Tech-2

NORAD ID: 39396
Origin: USA
Type: 3U CubeSat
Mass: 3 Kilograms
Inclination: 40.5°
Launched: November 20, 2013 - 1:15 UTC
Launch Vehicle: Minotaur I
Launch Site: Pad 0B, MARS, Wallops
Re-Entry Prediction: April 3, 2015 - 02:44 UTC +/- 480 Minutes
Re-Entry Zone: Unknown

The ORS Tech 2 satellite, 3U in size, demonstrated a multi-mission satellite bus in orbit that could be used for a variety of future applications. The payload was built by Johns Hopkins University.

>>>ORS-3 Launch Info