Showing default

ORBCOMM FM 115, 41186

Orbit data source: Space-Track

ORBCOMM FM 115, 41186 is a payload satellite owned by Orbcomm (US) in LEO that was launched on Tue, 22 Dec 2015 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.

Loading next visibility...
Identifier
41186, 2015-081H
Orbit
LEO
Country
Flag of USUS / ORB
Related 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)
2015-12-22 (10 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 ORBCOMM FM 115
1 41186U 15081H   25257.54017506  .00000486  00000-0  12892-3 0  9997
2 41186  46.9999 334.5501 0000543 207.1077 152.9782 14.62648770520854
Epoch: 2025-09-14T12:57Z
TLE epoch observation values (Epoch: 2025-09-14T12:57:51.125Z)
Latitude
-0.00001°
Longitude
146.32936°
Altitude
685.192 km
Speed
7.515 km/s
True Right ascension
22h 18m 12s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
00:35:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
686.255 km
Perigee altitude
685.488 km
Semi-major axis
7,064.008 km
Eccentricity
0.00005
Inclination
46.9999°
RAAN
334.5501°
Arg. of periapsis
207.1077°
True anomaly
152.98103°
Mean anomaly
152.9782°
Eccentric anomaly
152.97961°
Mean motion
3.65566 °/min
Orbital period
98.48 mins
BSTAR
0.00012892
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|