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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
68627 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Edit Sat Name
Focus sentinelFocus sentinel
Create New Watchlist
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: 1 day ago
TLE from 1 day ago
0 OBJECT A
1 68627U 26074A 26143.52957909 .00005546 00000-0 23886-3 0 9990
2 68627 60.0176 272.9419 0023069 355.7091 4.3788 15.23746659 7022Epoch: 2026-05-23T12:42Z
TLE epoch observation values (Epoch: 2026-05-23T12:42:35.633Z)
Latitude
0.00001°
Longitude
-158.85133°
Altitude
480.343 km
Speed
7.635 km/s
True Right ascension
18h 11m 46s
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
09:40:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.605 km
Perigee altitude
477.899 km
Semi-major axis
6,871.889 km
Eccentricity
0.00231
Inclination
60.0176°
RAAN
272.9419°
Arg. of periapsis
355.7091°
True anomaly
4.39904°
Mean anomaly
4.3788°
Eccentric anomaly
4.38891°
Mean motion
3.81003 °/min
Orbital period
94.49 mins
BSTAR
0.00023886
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #74 in the year 2026 (2026-04-07 UTC)
Did you know?
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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-25 10:32:02.044Z | 225.444° WSW | 2026-05-25 10:35:02.044Z | 259.874° W | 41.431° | 2026-05-25 10:39:02.044Z | 34.705° NE |
| 4 mins | 2026-05-25 17:11:02.044Z | 9.665° NNE | 2026-05-25 17:12:02.044Z | 28.351° NE | 16.971° | 2026-05-25 17:15:02.044Z | 81.075° E |
| 6 mins | 2026-05-25 18:48:02.044Z | 304.978° NW | 2026-05-25 18:50:02.044Z | 259.247° W | 37.278° | 2026-05-25 18:54:02.044Z | 158.908° S |
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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|