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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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, 5.3 m
Radar Cross Section
2.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 ORBCOMM FM 104
1 40090U 14040E 26263.11385297 .00000212 00000-0 83777-4 0 9998
2 40090 47.0055 42.6553 0016047 150.1449 210.0355 14.57363741647692Epoch: 2026-09-20T02:43Z
TLE epoch observation values (Epoch: 2026-09-20T02:43:56.896Z)
Latitude
-0°
Longitude
2.65554°
Altitude
711.754 km
Speed
7.496 km/s
True Right ascension
02h 50m 37s
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
03:55:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
714.295 km
Perigee altitude
691.569 km
Semi-major axis
7,081.069 km
Eccentricity
0.0016
Inclination
47.0055°
RAAN
42.6553°
Arg. of periapsis
150.1449°
True anomaly
209.94362°
Mean anomaly
210.0355°
Eccentric anomaly
209.98954°
Mean motion
3.64246 °/min
Orbital period
98.83 mins
BSTAR
0.000083777
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-20 11:06:30.213Z | 168.251° S | 2026-09-20 11:09:30.213Z | 129.694° SE | 16.48° | 2026-09-20 11:11:30.213Z | 103.376° ESE |
| 8 mins | 2026-09-20 12:48:30.213Z | 231.114° WSW | 2026-09-20 12:52:30.213Z | 119.487° SE | 72.785° | 2026-09-20 12:56:30.213Z | 64.816° ENE |
| 8 mins | 2026-09-20 14:32:30.213Z | 281.012° WNW | 2026-09-20 14:36:30.213Z | 0.282° NNE | 41.95° | 2026-09-20 14:40:30.213Z | 57.284° ENE |
| 7 mins | 2026-09-20 16:17:30.213Z | 310.275° NW | 2026-09-20 16:20:30.213Z | 9.278° NNE | 37.87° | 2026-09-20 16:24:30.213Z | 72.939° E |
| 8 mins | 2026-09-20 18:00:30.213Z | 300.484° NW | 2026-09-20 18:04:30.213Z | 31.622° NE | 79.219° | 2026-09-20 18:08:30.213Z | 113.209° SE |
| 6 mins | 2026-09-20 19:45:30.213Z | 260.598° W | 2026-09-20 19:47:30.213Z | 226.838° WSW | 25.352° | 2026-09-20 19:51:30.213Z | 169.82° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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