Showing default

CELTEE 1, 41850

Orbit data source: Space-Track

CELTEE 1, 41850 is a payload satellite owned by AFRL/RV (US) in SSO that was launched on Fri, 11 Nov 2016 UTC via an ATLAS V 401 launch vehicle from the Air Force Western Test Range (AFWTR). 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
41850, 2016-067C
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
M42 Tech
Mission
Operational Defense Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2016-11-11 (9 years ago)
Launch vehicle
ATLAS V 401
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 CELTEE 1
1 41850U 16067C   25239.49418373  .00006306  00000-0  33833-3 0  9996
2 41850  98.1027  81.2315 0002003 122.2599 237.8826 15.15348050481339
Epoch: 2025-08-27T11:51Z
TLE epoch observation values (Epoch: 2025-08-27T11:51:37.474Z)
Latitude
0.00001°
Longitude
-72.64538°
Altitude
523.72 km
Speed
7.601 km/s
True Right ascension
05h 24m 55s
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
16:42:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
518.306 km
Perigee altitude
515.544 km
Semi-major axis
6,895.062 km
Eccentricity
0.0002
Inclination
98.1027°
RAAN
81.2315°
Arg. of periapsis
122.2599°
True anomaly
237.86316°
Mean anomaly
237.8826°
Eccentric anomaly
237.87288°
Mean motion
3.79084 °/min
Orbital period
94.97 mins
BSTAR
0.00033833
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
|