OBJECT B, 59774
Orbit data source: Space-Track
OBJECT B, 59774 is a payload satellite owned by Sputniks (CIS) in SSO that was launched on Thu, 16 May 2024 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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59774 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Sputniks
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 OBJECT B
1 59774U 24092B 26318.33465828 .00011012 00000-0 36673-3 0 9991
2 59774 97.6678 92.0092 0008574 20.5636 339.5948 15.31273260138491Epoch: 2026-11-14T08:01Z
TLE epoch observation values (Epoch: 2026-11-14T08:01:54.475Z)
Latitude
-0.00001°
Longitude
-81.90871°
Altitude
469.605 km
Speed
7.634 km/s
True Right ascension
06h 08m 02s
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
09:37:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.845 km
Perigee altitude
463.104 km
Semi-major axis
6,847.112 km
Eccentricity
0.00086
Inclination
97.6678°
RAAN
92.0092°
Arg. of periapsis
20.5636°
True anomaly
339.56051°
Mean anomaly
339.5948°
Eccentric anomaly
339.57766°
Mean motion
3.83073 °/min
Orbital period
93.98 mins
BSTAR
0.00036673
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Other satellites on launch #92 in the year 2024 (2024-05-16 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 B 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 | 2026-11-14 21:09:11.240Z | 50.285° ENE | 2026-11-14 21:11:11.240Z | 86.535° E | 18.957° | 2026-11-14 21:13:11.240Z | 129.419° SE |
| 4 mins | 2026-11-14 22:43:11.240Z | 324.354° NNW | 2026-11-14 22:44:11.240Z | 302.016° NW | 22.109° | 2026-11-14 22:47:11.240Z | 239.731° WSW |
| 5 mins | 2026-11-15 09:16:11.240Z | 182.384° SSW | 2026-11-15 09:18:11.240Z | 295.196° NW | 62.455° | 2026-11-15 09:21:11.240Z | 341.964° 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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