Showing default

ORBCOMM FM 116, 41189

Orbit data source: Space-Track

ORBCOMM FM 116, 41189 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
41189, 2015-081L
Orbit
LEO
Country
Flag of USUS / ORB
Related business
Manufacturer
SNC Louisville
Mission
Operational Commercial Communications
Bus & Motor
SN-100A, Unknown motor
Mass
172 kg wet, 158 kg dry
Launch date (UTC)
2015-12-22 (11 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, 5.3 m
Radar Cross Section
2.222 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 ORBCOMM FM 116
1 41189U 15081L   26193.23026491  .00000069  00000-0  50766-4 0  9999
2 41189  47.0013 152.2072 0001450 221.9214 138.1561 14.58903801562591
Epoch: 2026-07-12T05:31Z
TLE epoch observation values (Epoch: 2026-07-12T05:31:34.888Z)
Latitude
-0°
Longitude
139.17972°
Altitude
697.695 km
Speed
7.508 km/s
True Right ascension
10h 08m 49s
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
07:52:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
698.977 km
Perigee altitude
696.925 km
Semi-major axis
7,076.088 km
Eccentricity
0.00015
Inclination
47.0013°
RAAN
152.2072°
Arg. of periapsis
221.9214°
True anomaly
138.16718°
Mean anomaly
138.1561°
Eccentric anomaly
138.16164°
Mean motion
3.64631 °/min
Orbital period
98.73 mins
BSTAR
0.000050766
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
|