OBJECT A, 101318
Orbit data source: Space-Track
OBJECT A, 101318 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Sat, 07 Nov 2026 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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101318 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT A
1 A1318U 26252A 26312.06709414 .00000063 00000-0 00000-0 0 9994
2 A1318 65.2194 187.1847 0017055 101.5877 235.8792 2.11672786 12Epoch: 2026-11-08T01:36Z
TLE epoch observation values (Epoch: 2026-11-08T01:36:36.933Z)
Latitude
-20.61995°
Longitude
105.78501°
Altitude
19,274.887 km
Speed
3.94 km/s
True Right ascension
11h 48m 48s
True Declination
-20° 35' 19"
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
11:58:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,287.887 km
Perigee altitude
19,200.489 km
Semi-major axis
25,622.325 km
Eccentricity
0.00171
Inclination
65.2194°
RAAN
187.1847°
Arg. of periapsis
101.5877°
True anomaly
235.7176°
Mean anomaly
235.8792°
Eccentric anomaly
235.79838°
Mean motion
0.52919 °/min
Orbital period
680.28 mins
BSTAR
0
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Other satellites on launch #252 in the year 2026 (2026-11-07 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. |
|---|---|---|---|---|---|---|---|
| 271 mins | 2026-11-10 01:38:11.636Z | 320.457° NNW | 2026-11-10 03:58:11.636Z | 271.124° WNW | 71.173° | 2026-11-10 06:09:11.636Z | 198.17° SSW |
| 119 mins | 2026-11-10 11:49:11.636Z | 79.773° E | 2026-11-10 12:49:11.636Z | 50.046° ENE | 19.647° | 2026-11-10 13:48:11.636Z | 22.994° NE |
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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