Showing default

ORBCOMM FM 20, 25416

Orbit data source: Space-Track

ORBCOMM FM 20, 25416 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.

Loading next visibility...
Identifier
25416, 1998-046D
Orbit
LEO
Country
Flag of USUS / ORB
Related business
Manufacturer
OSC-Germantown
Mission
Operational Commercial Communications
Bus & Motor
MICROSTAR, Unknown motor
Mass
42 kg wet, 42 kg dry
Launch date (UTC)
1998-08-02 (27 years ago)
Launch vehicle
PEGASUS XL/HAPS
Launch site
Pegasus Launch, Eastern Range Air Space (ERAS)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 2 Pan, 2.1 m
Radar Cross Section
1.484 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 ORBCOMM FM 20
1 25416U 98046D   25243.53566354  .00001715  00000-0  61654-3 0  9997
2 25416  44.9934 184.4070 0002777 318.5228  41.5409 14.37334625415101
Epoch: 2025-08-31T12:51Z
TLE epoch observation values (Epoch: 2025-08-31T12:51:21.329Z)
Latitude
-0.00002°
Longitude
11.6139°
Altitude
765.832 km
Speed
7.474 km/s
True Right ascension
12h 17m 37s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
12:34:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
770.85 km
Perigee altitude
766.88 km
Semi-major axis
7,147.002 km
Eccentricity
0.00028
Inclination
44.9934°
RAAN
184.407°
Arg. of periapsis
318.5228°
True anomaly
41.56201°
Mean anomaly
41.5409°
Eccentric anomaly
41.55145°
Mean motion
3.59217 °/min
Orbital period
100.22 mins
BSTAR
0.00061654
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|