DECAYED

OBJECT L, 43859 (Decayed)

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT L, 43859 was a satellite owned by NASA GRC (US) in LEO that was launched on Sun, 16 Dec 2018 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.

Not visible in the next 10 days
Identifier
43859, 2018-104L
Orbit
Decayed
Country
Flag of USUS
Related business
None
Manufacturer
NASA GRC
Mission
Decayed Civil Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
2.91 kg wet, 2.91 kg dry
Launch date (UTC)
2018-12-16 (7 years ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Unknown
Shape & HBR
Box + 4 Pan, 0.3 m
Radar Cross Section
0.066 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year ago
0 OBJECT L
1 43859U 18104L   24194.91423858  .09173232 -15042-5  34830-3 0  9999
2 43859  84.9829 254.0101 0013879 258.4364 101.5385 16.42702273311208
Epoch: 2024-07-12T21:56Z
TLE epoch observation values (Epoch: 2024-07-12T21:56:30.213Z)
Latitude
Longitude
-6.39948°
Altitude
163.766 km
Speed
7.807 km/s
True Right ascension
16h 56m 02s
True Declination
0° 00' 00"
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
18:11:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
164.406 km
Perigee altitude
146.27 km
Semi-major axis
6,533.475 km
Eccentricity
0.00139
Inclination
84.9829°
RAAN
254.0101°
Arg. of periapsis
258.4364°
True anomaly
101.69427°
Mean anomaly
101.5385°
Eccentric anomaly
101.61639°
Mean motion
4.10986 °/min
Orbital period
87.59 mins
BSTAR
0.0003483
Loading maneuver chart data...
Computing Atmospheric mass density...

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