ORBCOMM FM 106, 40088
Orbit data source: Space-Track
ORBCOMM FM 106, 40088 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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40088 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, 6.5 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 106
1 40088U 14040C 25260.01709029 .00000838 00000-0 17080-3 0 9990
2 40088 47.0596 118.2157 0016466 134.5307 225.6932 14.69646025596983Epoch: 2025-09-17T00:24Z
TLE epoch observation values (Epoch: 2025-09-17T00:24:36.601Z)
Latitude
0°
Longitude
115.86411°
Altitude
670.528 km
Speed
7.519 km/s
True Right ascension
07h 52m 51s
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
13:34:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
675.024 km
Perigee altitude
651.835 km
Semi-major axis
7,041.567 km
Eccentricity
0.00165
Inclination
47.0596°
RAAN
118.2157°
Arg. of periapsis
134.5307°
True anomaly
225.55837°
Mean anomaly
225.6932°
Eccentric anomaly
225.62576°
Mean motion
3.67315 °/min
Orbital period
98.01 mins
BSTAR
0.0001708
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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 106 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 | 2025-09-17 22:01:35.163Z | 303.765° NW | 2025-09-17 22:05:35.163Z | 7.403° NNE | 34.406° | 2025-09-17 22:09:35.163Z | 84.204° E |
| 7 mins | 2025-09-17 23:45:35.163Z | 289.762° WNW | 2025-09-17 23:48:35.163Z | 216.712° SW | 42.042° | 2025-09-17 23:52:35.163Z | 133.837° SE |
| 7 mins | 2025-09-18 17:24:35.163Z | 223.575° SW | 2025-09-18 17:27:35.163Z | 140.192° SSE | 42.358° | 2025-09-18 17:31:35.163Z | 66.835° ENE |
| 7 mins | 2025-09-18 19:07:35.163Z | 283.517° WNW | 2025-09-18 19:10:35.163Z | 353.345° N | 34.314° | 2025-09-18 19:14:35.163Z | 56.334° ENE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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