OBJECT E, 68631
Orbit data source: Space-Track
OBJECT E, 68631 is a satellite owned by USSF SMC (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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68631 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NGIS FSG
Mission
Operational spacecraft
Bus & Motor
ORION 38, Unknown motor
Mass
~500 kg wet, ~500 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: 2 days ago
TLE from 2 days ago
0 OBJECT E
1 68631U 26074E 26143.50785001 .00003063 00000-0 13504-3 0 9993
2 68631 60.0209 272.8512 0023960 6.6560 353.4834 15.24315458 7020Epoch: 2026-05-23T12:11Z
TLE epoch observation values (Epoch: 2026-05-23T12:11:18.240Z)
Latitude
-0.00004°
Longitude
-151.09817°
Altitude
478.086 km
Speed
7.637 km/s
True Right ascension
18h 11m 24s
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
09:40:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.503 km
Perigee altitude
475.581 km
Semi-major axis
6,870.179 km
Eccentricity
0.0024
Inclination
60.0209°
RAAN
272.8512°
Arg. of periapsis
6.656°
True anomaly
353.45215°
Mean anomaly
353.4834°
Eccentric anomaly
353.46778°
Mean motion
3.81146 °/min
Orbital period
94.45 mins
BSTAR
0.00013504
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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 | 2026-05-25 09:59:11.941Z | 196.583° SSW | 2026-05-25 10:02:11.941Z | 122.184° SE | 36.582° | 2026-05-25 10:05:11.941Z | 52.133° ENE |
| 6 mins | 2026-05-25 18:14:11.941Z | 328.946° NNW | 2026-05-25 18:17:11.941Z | 83.716° E | 41.83° | 2026-05-25 18:20:11.941Z | 132.325° SE |
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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