OBJECT J, 61743
Orbit data source: Space-Track
OBJECT J, 61743 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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61743 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 J
1 61743U 24199J 26309.92424755 .00001723 00000-0 14871-3 0 9991
2 61743 97.3131 140.6866 0005522 313.1964 46.8798 14.98459861153218Epoch: 2026-11-05T22:10Z
TLE epoch observation values (Epoch: 2026-11-05T22:10:54.988Z)
Latitude
0°
Longitude
122.80625°
Altitude
572.095 km
Speed
7.576 km/s
True Right ascension
09h 22m 44s
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
10:38:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.481 km
Perigee altitude
564.809 km
Semi-major axis
6,946.782 km
Eccentricity
0.00055
Inclination
97.3131°
RAAN
140.6866°
Arg. of periapsis
313.1964°
True anomaly
46.92601°
Mean anomaly
46.8798°
Eccentric anomaly
46.9029°
Mean motion
3.74859 °/min
Orbital period
96.04 mins
BSTAR
0.00014871
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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 J 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 | 2026-11-07 01:59:49.221Z | 359.497° N | 2026-11-07 02:02:49.221Z | 279.498° WNW | 57.473° | 2026-11-07 02:05:49.221Z | 209.604° SW |
| 6 mins | 2026-11-07 12:46:49.221Z | 157.318° SSE | 2026-11-07 12:49:49.221Z | 41.389° NE | 68.066° | 2026-11-07 12:52:49.221Z | 353.897° N |
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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