Showing default

ORBCOMM FM 16, 25417

Orbit data source: Space-Track

ORBCOMM FM 16, 25417 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
25417, 1998-046E
Orbit
LEO
Country
Flag of USUS / ORB
Related business
Manufacturer
OSC-Germantown
Mission
Non-operational Commercial Communications
Bus & Motor
MICROSTAR, Unknown motor
Mass
42 kg wet, 42 kg dry
Launch date (UTC)
1998-08-02 (28 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, 4.2 m
Radar Cross Section
1.484 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 ORBCOMM FM 16
1 25417U 98046E   26259.24529680  .00000818  00000-0  30098-3 0  9996
2 25417  44.9927 164.5333 0004901  53.6976 306.4326 14.40211797469976
Epoch: 2026-09-16T05:53Z
TLE epoch observation values (Epoch: 2026-09-16T05:53:13.643Z)
Latitude
0.00005°
Longitude
81.02685°
Altitude
755.721 km
Speed
7.479 km/s
True Right ascension
10h 58m 08s
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
18:36:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
762.846 km
Perigee altitude
755.849 km
Semi-major axis
7,137.485 km
Eccentricity
0.00049
Inclination
44.9927°
RAAN
164.5333°
Arg. of periapsis
53.6976°
True anomaly
306.3874°
Mean anomaly
306.4326°
Eccentric anomaly
306.41°
Mean motion
3.59936 °/min
Orbital period
100.02 mins
BSTAR
0.00030098
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|