Showing default

ORBCOMM FM 104, 40090

Orbit data source: Space-Track

ORBCOMM FM 104, 40090 is a payload satellite owned by Orbcomm (US) in LEO that was launched on Mon, 14 Jul 2014 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
40090, 2014-040E
Orbit
LEO
Country
Flag of USUS / ORB
Related business
Manufacturer
SNC Louisville
Mission
Non-operational Commercial Communications
Bus & Motor
SN-100A, Unknown motor
Mass
172 kg wet, 158 kg dry
Launch date (UTC)
2014-07-14 (11 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan + 1 Ant, 6.5 m
Radar Cross Section
2.222 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 ORBCOMM FM 104
1 40090U 14040E   25260.24779597  .00000477  00000-0  14310-3 0  9997
2 40090  47.0067 337.1158 0017307 265.1212  94.7697 14.56773785594041
Epoch: 2025-09-17T05:56Z
TLE epoch observation values (Epoch: 2025-09-17T05:56:49.571Z)
Latitude
-0.00003°
Longitude
-108.51725°
Altitude
704.866 km
Speed
7.504 km/s
True Right ascension
22h 28m 27s
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
13:34:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
717.102 km
Perigee altitude
692.585 km
Semi-major axis
7,082.98 km
Eccentricity
0.00173
Inclination
47.0067°
RAAN
337.1158°
Arg. of periapsis
265.1212°
True anomaly
94.9673°
Mean anomaly
94.7697°
Eccentric anomaly
94.8685°
Mean motion
3.64099 °/min
Orbital period
98.87 mins
BSTAR
0.0001431
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|