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.
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40090 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
US / ORBRelated 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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan + 1 Ant, 10.3 m
Radar Cross Section
2.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 ORBCOMM FM 104
1 40090U 14040E 25302.28882300 .00000894 00000-0 23490-3 0 9997
2 40090 47.0033 138.9926 0015877 98.2598 262.0088 14.56886047600178Epoch: 2025-10-29T06:55Z
TLE epoch observation values (Epoch: 2025-10-29T06:55:54.307Z)
Latitude
-0.00002°
Longitude
-2.8478°
Altitude
705.042 km
Speed
7.504 km/s
True Right ascension
09h 15m 58s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
22:02:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
715.725 km
Perigee altitude
693.235 km
Semi-major axis
7,082.617 km
Eccentricity
0.00159
Inclination
47.0033°
RAAN
138.9926°
Arg. of periapsis
98.2598°
True anomaly
261.82868°
Mean anomaly
262.0088°
Eccentric anomaly
261.91873°
Mean motion
3.64127 °/min
Orbital period
98.87 mins
BSTAR
0.0002349
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Other satellites on launch #40 in the year 2014 (2014-07-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ORBCOMM FM 104 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-30 16:02:52.041Z | 221.8° SW | 2025-10-30 16:05:52.041Z | 174.688° S | 40.359° | 2025-10-30 16:10:52.041Z | 67.282° ENE |
| 7 mins | 2025-10-30 17:46:52.041Z | 277.987° WNW | 2025-10-30 17:49:52.041Z | 335.433° NNW | 35.787° | 2025-10-30 17:53:52.041Z | 54.032° ENE |
| 8 mins | 2025-10-30 19:30:52.041Z | 303.092° NW | 2025-10-30 19:34:52.041Z | 17.238° NNE | 30.405° | 2025-10-30 19:38:52.041Z | 71.76° E |
| 8 mins | 2025-10-30 21:14:52.041Z | 302.846° NW | 2025-10-30 21:18:52.041Z | 51.153° ENE | 42.656° | 2025-10-30 21:22:52.041Z | 107.346° ESE |
| 7 mins | 2025-10-30 22:58:52.041Z | 273.165° WNW | 2025-10-30 23:01:52.041Z | 222.506° SW | 27.155° | 2025-10-30 23:05:52.041Z | 162.363° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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