OBJECT A, 68627
Orbit data source: Space-Track
OBJECT A, 68627 is a satellite owned by Auburn U (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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68627 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Endurosat
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, AOCS
Mass
3.9 kg wet, 3.9 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: 13 hours ago
TLE from 13 hours ago
0 OBJECT A
1 68627U 26074A 26140.37995220 .00005012 00000-0 21733-3 0 9995
2 68627 60.0186 285.0146 0022429 353.3054 6.7723 15.23709357 6542Epoch: 2026-05-20T09:07Z
TLE epoch observation values (Epoch: 2026-05-20T09:07:07.870Z)
Latitude
-0.00001°
Longitude
-89.80854°
Altitude
480.956 km
Speed
7.634 km/s
True Right ascension
19h 00m 03s
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
07:04:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.277 km
Perigee altitude
478.451 km
Semi-major axis
6,872.001 km
Eccentricity
0.00224
Inclination
60.0186°
RAAN
285.0146°
Arg. of periapsis
353.3054°
True anomaly
6.80269°
Mean anomaly
6.7723°
Eccentric anomaly
6.78749°
Mean motion
3.80994 °/min
Orbital period
94.49 mins
BSTAR
0.00021733
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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 A 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 12:04:51.563Z | 249.15° W | 2026-05-21 12:06:51.563Z | 320.443° NNW | 36.645° | 2026-05-21 12:09:51.563Z | 26.41° NE |
| 5 mins | 2026-05-21 18:41:51.563Z | 358.754° N | 2026-05-21 18:43:51.563Z | 40.589° NE | 21.668° | 2026-05-21 18:46:51.563Z | 94.331° ESE |
| 5 mins | 2026-05-21 20:19:51.563Z | 286.74° WNW | 2026-05-21 20:21:51.563Z | 228.284° WSW | 29.821° | 2026-05-21 20:24:51.563Z | 172.571° S |
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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