Showing default

MISR-C-2, 68633

Orbit data source: Space-Track

MISR-C-2, 68633 is a payload satellite owned by SOCOM (US) in LEO that was launched on Tue, 07 Apr 2026 UTC via an MINOTAUR IV 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
68633, 2026-074G
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
LANL?
Mission
Operational spacecraft
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2026-04-07 (2 months ago)
Launch vehicle
MINOTAUR IV
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 MISR-C-2
1 68633U 26074G   26144.06505844  .00007907  00000-0  31693-3 0  9992
2 68633  60.0221 270.4214 0024985  14.9980 345.1837 15.25617054  7103
Epoch: 2026-05-24T01:33Z
TLE epoch observation values (Epoch: 2026-05-24T01:33:41.049Z)
Latitude
0.00004°
Longitude
5.32783°
Altitude
473.95 km
Speed
7.639 km/s
True Right ascension
18h 01m 41s
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
09:39:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.288 km
Perigee altitude
470.977 km
Semi-major axis
6,866.27 km
Eccentricity
0.0025
Inclination
60.0221°
RAAN
270.4214°
Arg. of periapsis
14.998°
True anomaly
345.11026°
Mean anomaly
345.1837°
Eccentric anomaly
345.147°
Mean motion
3.81471 °/min
Orbital period
94.37 mins
BSTAR
0.00031693
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
|