ORBCOMM FM 7, 25119
Orbit data source: Space-Track
ORBCOMM FM 7, 25119 is a payload satellite owned by Orbcomm (US) in LEO that was launched on Tue, 23 Dec 1997 UTC via a PEGASUS XL/HAPS launch vehicle from the Pegasus Launch, Eastern Range Air Space (ERAS). 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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25119 intel report (Beta)
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Identifier
Orbit
Country
US / ORBRelated business
Manufacturer
OSC-Germantown
Mission
Non-operational Commercial Communications
Bus & Motor
MICROSTAR, Unknown motor
Mass
42 kg wet, 42 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 4.2 m
Radar Cross Section
1.484 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ORBCOMM FM 7
1 25119U 97084H 26171.31687679 .00000814 00000-0 25817-3 0 9999
2 25119 45.0144 38.3794 0002397 297.9596 62.1014 14.47576321494832Epoch: 2026-06-20T07:36Z
TLE epoch observation values (Epoch: 2026-06-20T07:36:18.154Z)
Latitude
0.00002°
Longitude
15.77054°
Altitude
732.779 km
Speed
7.491 km/s
True Right ascension
02h 33m 31s
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
00:39:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
736.831 km
Perigee altitude
733.421 km
Semi-major axis
7,113.263 km
Eccentricity
0.00024
Inclination
45.0144°
RAAN
38.3794°
Arg. of periapsis
297.9596°
True anomaly
62.12568°
Mean anomaly
62.1014°
Eccentric anomaly
62.11354°
Mean motion
3.61776 °/min
Orbital period
99.51 mins
BSTAR
0.00025817
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Other satellites on launch #84 in the year 1997 (1997-12-23 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 7 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 | 2026-06-22 16:04:13.013Z | 165.749° S | 2026-06-22 16:07:13.013Z | 129.914° SE | 13.866° | 2026-06-22 16:09:13.013Z | 106.145° ESE |
| 8 mins | 2026-06-22 17:47:13.013Z | 223.686° SW | 2026-06-22 17:50:13.013Z | 174.237° S | 40.298° | 2026-06-22 17:55:13.013Z | 71.64° E |
| 9 mins | 2026-06-22 19:31:13.013Z | 272.165° WNW | 2026-06-22 19:35:13.013Z | 345.859° N | 39.759° | 2026-06-22 19:40:13.013Z | 66.16° ENE |
| 8 mins | 2026-06-22 21:17:13.013Z | 300.623° NW | 2026-06-22 21:20:13.013Z | 4.314° NNE | 37.719° | 2026-06-22 21:25:13.013Z | 83.325° E |
| 9 mins | 2026-06-22 23:01:13.013Z | 291.48° WNW | 2026-06-22 23:05:13.013Z | 176.771° S | 44.475° | 2026-06-22 23:10:13.013Z | 120.201° SE |
| 6 mins | 2026-06-23 00:46:13.013Z | 261.729° W | 2026-06-23 00:49:13.013Z | 219.322° SW | 20.082° | 2026-06-23 00:52:13.013Z | 179.367° 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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