OBJECT AN, 61771
Orbit data source: Space-Track
OBJECT AN, 61771 is a payload satellite in SSO that was launched on Mon, 04 Nov 2024 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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61771 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Manufacturer
Sputniks
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 OBJECT AN
1 61771U 24199AN 26309.92114576 .00115522 00000-0 72815-3 0 9994
2 61771 97.2638 190.5939 0007784 104.7507 255.4622 15.76286678156605Epoch: 2026-11-05T22:06Z
TLE epoch observation values (Epoch: 2026-11-05T22:06:26.993Z)
Latitude
-0.00003°
Longitude
173.83326°
Altitude
345.46 km
Speed
7.701 km/s
True Right ascension
12h 42m 22s
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
10:37:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
343.085 km
Perigee altitude
332.63 km
Semi-major axis
6,715.994 km
Eccentricity
0.00078
Inclination
97.2638°
RAAN
190.5939°
Arg. of periapsis
104.7507°
True anomaly
255.37588°
Mean anomaly
255.4622°
Eccentric anomaly
255.41904°
Mean motion
3.94346 °/min
Orbital period
91.29 mins
BSTAR
0.00072815
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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 AN 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-06 16:31:33.741Z | 191.488° SSW | 2026-11-06 16:33:33.741Z | 272.094° WNW | 43.816° | 2026-11-06 16:35:33.741Z | 331.91° NNW |
| 4 mins | 2026-11-07 05:08:33.741Z | 6.611° NNE | 2026-11-07 05:09:33.741Z | 353.41° N | 58.699° | 2026-11-07 05:12:33.741Z | 196.252° SSW |
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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