OBJECT A, 68627
Orbit data source: Space-Track
OBJECT A, 68627 is a satellite owned by USAF STP (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
Aegis Aerospace
Mission
Operational spacecraft
Bus & Motor
STPSAT7, AOCS
Mass
~100 kg wet, ~100 kg dry
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 A
1 68627U 26074A 26099.55814991 .00009079 00000-0 39165-3 0 9998
2 68627 60.0170 81.4166 0015862 304.6447 55.3137 15.23130172 325Epoch: 2026-04-09T13:23Z
TLE epoch observation values (Epoch: 2026-04-09T13:23:44.152Z)
Latitude
-0.00001°
Longitude
42.67819°
Altitude
491.811 km
Speed
7.623 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
02:17:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.51 km
Perigee altitude
484.704 km
Semi-major axis
6,873.744 km
Eccentricity
0.00159
Inclination
60.017°
RAAN
81.4166°
Arg. of periapsis
304.6447°
True anomaly
55.46333°
Mean anomaly
55.3137°
Eccentric anomaly
55.3885°
Mean motion
3.80849 °/min
Orbital period
94.53 mins
BSTAR
0.00039165
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-10 00:34:33.462Z | 194.248° SSW | 2026-04-10 00:37:33.462Z | 104.613° ESE | 36.045° | 2026-04-10 00:40:33.462Z | 50.881° ENE |
| 4 mins | 2026-04-10 02:13:33.462Z | 290.795° WNW | 2026-04-10 02:15:33.462Z | 330.544° NNW | 17.568° | 2026-04-10 02:17:33.462Z | 4.386° NNE |
| 5 mins | 2026-04-10 08:50:33.462Z | 333.327° NNW | 2026-04-10 08:52:33.462Z | 68.427° E | 42.625° | 2026-04-10 08:55:33.462Z | 132.029° 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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