OBJECT J, 68635
Orbit data source: Space-Track
OBJECT J, 68635 is a satellite owned by Texas A&M (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). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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68635 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Texas A&M
Mission
Operational spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 OBJECT J
1 68635U 26074J 26138.45427486 .00006056 00000-0 25277-3 0 9990
2 68635 60.0228 292.2233 0024343 359.8092 0.2975 15.24644357 6250Epoch: 2026-05-18T10:54Z
TLE epoch observation values (Epoch: 2026-05-18T10:54:09.347Z)
Latitude
-0.00005°
Longitude
-107.45798°
Altitude
476.73 km
Speed
7.637 km/s
True Right ascension
19h 28m 53s
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
09:53:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.775 km
Perigee altitude
474.332 km
Semi-major axis
6,869.19 km
Eccentricity
0.00243
Inclination
60.0228°
RAAN
292.2233°
Arg. of periapsis
359.8092°
True anomaly
0.29895°
Mean anomaly
0.2975°
Eccentric anomaly
0.29823°
Mean motion
3.81228 °/min
Orbital period
94.43 mins
BSTAR
0.00025277
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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.OBJECT J 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-19 12:14:32.542Z | 215.968° SW | 2026-05-19 12:17:32.542Z | 77.351° E | 44.802° | 2026-05-19 12:20:32.542Z | 40.005° NE |
| 6 mins | 2026-05-19 20:29:32.542Z | 314.498° NW | 2026-05-19 20:32:32.542Z | 184.6° SSW | 41.711° | 2026-05-19 20:35:32.542Z | 149.943° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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