OBJECT E, 68631
Orbit data source: Space-Track
OBJECT E, 68631 is an American satellite 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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68631 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OBJECT E
1 68631U 26074E 26099.55697052 .00005224 00000-0 22476-3 0 9995
2 68631 60.0204 81.4157 0015950 319.1139 40.8744 15.23998738 328Epoch: 2026-04-09T13:22Z
TLE epoch observation values (Epoch: 2026-04-09T13:22:02.252Z)
Latitude
-0.00004°
Longitude
43.10301°
Altitude
487.113 km
Speed
7.627 km/s
True Right ascension
05h 25m 39s
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
02:17:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.953 km
Perigee altitude
482.034 km
Semi-major axis
6,871.131 km
Eccentricity
0.0016
Inclination
60.0204°
RAAN
81.4157°
Arg. of periapsis
319.1139°
True anomaly
40.99419°
Mean anomaly
40.8744°
Eccentric anomaly
40.93428°
Mean motion
3.81067 °/min
Orbital period
94.47 mins
BSTAR
0.00022476
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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 E 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 | 2026-04-10 00:31:45.617Z | 196.209° SSW | 2026-04-10 00:34:45.617Z | 139.829° SSE | 34.978° | 2026-04-10 00:37:45.617Z | 55.661° ENE |
| 6 mins | 2026-04-10 08:46:45.617Z | 328.491° NNW | 2026-04-10 08:49:45.617Z | 31.353° NE | 41.643° | 2026-04-10 08:52:45.617Z | 128.736° SE |
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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