ORBCOMM FM 14, 25419
Orbit data source: Space-Track
ORBCOMM FM 14, 25419 is a payload satellite owned by Orbcomm (US) in LEO that was launched on Sun, 02 Aug 1998 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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25419 intel report (Beta)
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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 ORBCOMM FM 14
1 25419U 98046G 25344.63390074 .00002213 00000-0 74729-3 0 9998
2 25419 44.9956 57.9543 0002129 152.0935 208.0028 14.39567778429633Epoch: 2025-12-10T15:12Z
TLE epoch observation values (Epoch: 2025-12-10T15:12:49.023Z)
Latitude
-0.00005°
Longitude
110.14857°
Altitude
761.267 km
Speed
7.475 km/s
True Right ascension
03h 51m 49s
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
21:05:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
762.995 km
Perigee altitude
759.955 km
Semi-major axis
7,139.612 km
Eccentricity
0.00021
Inclination
44.9956°
RAAN
57.9543°
Arg. of periapsis
152.0935°
True anomaly
207.99135°
Mean anomaly
208.0028°
Eccentric anomaly
207.99707°
Mean motion
3.59775 °/min
Orbital period
100.06 mins
BSTAR
0.00074729
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Other satellites on launch #46 in the year 1998 (1998-08-02 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 14 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 | 2025-12-11 08:04:15.554Z | 212.78° SW | 2025-12-11 08:07:15.554Z | 157.704° S | 37.135° | 2025-12-11 08:12:15.554Z | 74.061° E |
| 8 mins | 2025-12-11 09:49:15.554Z | 268.905° W | 2025-12-11 09:52:15.554Z | 322.624° NNW | 41.132° | 2025-12-11 09:57:15.554Z | 64.616° ENE |
| 9 mins | 2025-12-11 11:34:15.554Z | 293.427° NW | 2025-12-11 11:38:15.554Z | 4.671° NNE | 37.355° | 2025-12-11 11:43:15.554Z | 79.62° E |
| 8 mins | 2025-12-11 13:20:15.554Z | 294.059° NW | 2025-12-11 13:23:15.554Z | 300.685° NW | 44.078° | 2025-12-11 13:28:15.554Z | 113.768° SE |
| 7 mins | 2025-12-11 15:05:15.554Z | 267.312° W | 2025-12-11 15:08:15.554Z | 223.387° SW | 24.465° | 2025-12-11 15:12:15.554Z | 167.558° 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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