DECAYED

MINOTAUR-C R/B, 42994 (Decayed)

Orbit data source: Space-Track

MINOTAUR-C R/B, 42994 was space debris in LEO originally from a launch on Tue, 31 Oct 2017 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

Not visible in the next 10 days
Identifier
42994, 2017-068H
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
OATK FSG Utah
Mission
Decayed spacecraft
Bus & Motor
ORION 38, Unknown motor
Mass
202 kg wet, 202 kg dry
Launch date (UTC)
2017-10-31 (8 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.7 m
Radar Cross Section
1.492 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 months ago

TLE from 8 months ago
0 MINOTAUR-C R/B
1 42994U 17068H   25003.91904544  .18667292  24924-5  23657-3 0  9999
2 42994  97.4256 138.4408 0010042 319.7263 137.3533 16.49219218399705
Epoch: 2025-01-03T22:03Z
TLE epoch observation values (Epoch: 2025-01-03T22:03:25.526Z)
Latitude
79.75225°
Longitude
-70.40514°
Altitude
159.551 km
Speed
7.815 km/s
True Right ascension
00h 16m 54s
True Declination
79° 41' 11"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
01:20:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
144.733 km
Perigee altitude
131.645 km
Semi-major axis
6,516.326 km
Eccentricity
0.001
Inclination
97.4256°
RAAN
138.4408°
Arg. of periapsis
319.7263°
True anomaly
137.43119°
Mean anomaly
137.3533°
Eccentric anomaly
137.39225°
Mean motion
4.12609 °/min
Orbital period
87.25 mins
BSTAR
0.00023657
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