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.
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68633 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LANL?
Mission
Operational spacecraft
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 MISR-C-2
1 68633U 26074G 26140.65712414 .00006773 00000-0 27375-3 0 9998
2 68633 60.0227 283.5192 0024383 12.7729 347.3964 15.25560072 6581Epoch: 2026-05-20T15:46Z
TLE epoch observation values (Epoch: 2026-05-20T15:46:15.525Z)
Latitude
-0.00008°
Longitude
168.64093°
Altitude
474.366 km
Speed
7.639 km/s
True Right ascension
18h 54m 04s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:56:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.046 km
Perigee altitude
471.561 km
Semi-major axis
6,866.44 km
Eccentricity
0.00244
Inclination
60.0227°
RAAN
283.5192°
Arg. of periapsis
12.7729°
True anomaly
347.33525°
Mean anomaly
347.3964°
Eccentric anomaly
347.36584°
Mean motion
3.81457 °/min
Orbital period
94.37 mins
BSTAR
0.00027375
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Other satellites on launch #74 in the year 2026 (2026-04-07 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.MISR-C-2 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-21 10:47:17.929Z | 169.366° S | 2026-05-21 10:49:17.929Z | 132.172° SE | 21.23° | 2026-05-21 10:52:17.929Z | 69.993° E |
| 5 mins | 2026-05-21 12:25:17.929Z | 269.176° W | 2026-05-21 12:27:17.929Z | 320.624° NNW | 25.957° | 2026-05-21 12:30:17.929Z | 18.153° NNE |
| 5 mins | 2026-05-21 19:02:17.929Z | 359.144° N | 2026-05-21 19:04:17.929Z | 62.018° ENE | 28.797° | 2026-05-21 19:07:17.929Z | 111.998° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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