OBJECT R, 68431
Orbit data source: Space-Track
OBJECT R, 68431 is a satellite in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 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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68431 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Aarhus University (DK)Manufacturer
Aarhus U.
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~5 kg wet, ~5 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: 11 hours ago
TLE from 11 hours ago
0 OBJECT R
1 68431U 26067R 26127.13577199 .00007037 00000-0 34442-3 0 9990
2 68431 97.4583 86.2517 0004186 116.4508 243.7156 15.18485444 5718Epoch: 2026-05-07T03:15Z
TLE epoch observation values (Epoch: 2026-05-07T03:15:30.699Z)
Latitude
-0.00005°
Longitude
172.38754°
Altitude
514.782 km
Speed
7.606 km/s
True Right ascension
05h 45m 00s
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
22:03:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.27 km
Perigee altitude
504.505 km
Semi-major axis
6,885.524 km
Eccentricity
0.00042
Inclination
97.4583°
RAAN
86.2517°
Arg. of periapsis
116.4508°
True anomaly
243.6726°
Mean anomaly
243.7156°
Eccentric anomaly
243.6941°
Mean motion
3.79872 °/min
Orbital period
94.77 mins
BSTAR
0.00034442
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Other satellites on launch #67 in the year 2026 (2026-03-30 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 R 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 | 2026-05-07 20:47:35.688Z | 134.048° SE | 2026-05-07 20:50:35.688Z | 61.612° ENE | 29.552° | 2026-05-07 20:53:35.688Z | 6.878° NNE |
| 5 mins | 2026-05-08 09:53:35.688Z | 32.933° NE | 2026-05-08 09:55:35.688Z | 117.154° SE | 38.939° | 2026-05-08 09:58:35.688Z | 177.637° 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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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