OBJECT AK, 61768
Orbit data source: Space-Track
OBJECT AK, 61768 is a satellite in SSO that was launched on Mon, 04 Nov 2024 UTC launched from the Vostochny Cosmodrome (VOSTO). 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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61768 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 OBJECT AK
1 61768U 24199AK 26127.90006326 .00017604 00000-0 33822-3 0 9996
2 61768 97.3017 2.2796 0007568 81.8468 278.3641 15.47978657128106Epoch: 2026-05-07T21:36Z
TLE epoch observation values (Epoch: 2026-05-07T21:36:05.465Z)
Latitude
-0.00001°
Longitude
172.51726°
Altitude
425.026 km
Speed
7.657 km/s
True Right ascension
00h 09m 07s
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
13:37:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
424.709 km
Perigee altitude
414.42 km
Semi-major axis
6,797.701 km
Eccentricity
0.00076
Inclination
97.3017°
RAAN
2.2796°
Arg. of periapsis
81.8468°
True anomaly
278.27829°
Mean anomaly
278.3641°
Eccentric anomaly
278.3212°
Mean motion
3.87258 °/min
Orbital period
92.96 mins
BSTAR
0.00033822
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Other satellites on launch #199 in the year 2024 (2024-11-04 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 AK Visibility
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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. |
|---|---|---|---|---|---|---|---|
| OBJECT AK is likely not visible in the next few days. |
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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