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   25258.22326538  .00000760  00000-0  18230-3 0  9998
2 41186  46.9997 331.3006 0000577 209.0190 151.0665 14.62651638520959
Epoch: 2025-09-15T05:21Z
TLE epoch observation values (Epoch: 2025-09-15T05:21:30.128Z)
Latitude
-0.00006°
Longitude
-103.50599°
Altitude
685.197 km
Speed
7.515 km/s
True Right ascension
22h 05m 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
17:03:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
686.27 km
Perigee altitude
685.455 km
Semi-major axis
7,063.999 km
Eccentricity
0.00006
Inclination
46.9997°
RAAN
331.3006°
Arg. of periapsis
209.019°
True anomaly
151.0697°
Mean anomaly
151.0665°
Eccentric anomaly
151.0681°
Mean motion
3.65567 °/min
Orbital period
98.48 mins
BSTAR
0.0001823
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
|