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, 10.3 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   26048.12442270  .00000835  00000-0  19507-3 0  9998
2 41186  46.9994 314.1461 0000308 111.6085 248.4835 14.63079464543635
Epoch: 2026-02-17T02:59Z
TLE epoch observation values (Epoch: 2026-02-17T02:59:10.121Z)
Latitude
-0.00003°
Longitude
122.24498°
Altitude
683.544 km
Speed
7.516 km/s
True Right ascension
20h 56m 35s
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
00:27:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
684.703 km
Perigee altitude
684.268 km
Semi-major axis
7,062.623 km
Eccentricity
0.00003
Inclination
46.9994°
RAAN
314.1461°
Arg. of periapsis
111.6085°
True anomaly
248.48022°
Mean anomaly
248.4835°
Eccentric anomaly
248.48186°
Mean motion
3.65674 °/min
Orbital period
98.45 mins
BSTAR
0.00019507
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
|