OBJECT Z, 57189
Orbit data source: Space-Track
OBJECT Z, 57189 is a payload satellite in SSO that was launched on Tue, 27 Jun 2023 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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57189 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Manufacturer
Sputniks
Mission
Operational Commercial Com/Met
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
2.98 kg wet, 2.98 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: 18 hours ago
TLE from 18 hours ago
0 OBJECT Z
1 57189U 23091Z 26314.19538854 .00025434 00000-0 62836-3 0 9990
2 57189 97.4946 26.9341 0004930 264.9553 95.1130 15.40467093187134Epoch: 2026-11-10T04:41Z
TLE epoch observation values (Epoch: 2026-11-10T04:41:21.569Z)
Latitude
-0.00008°
Longitude
-92.76683°
Altitude
448.147 km
Speed
7.643 km/s
True Right ascension
01h 47m 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
18:46:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.034 km
Perigee altitude
438.31 km
Semi-major axis
6,819.809 km
Eccentricity
0.00049
Inclination
97.4946°
RAAN
26.9341°
Arg. of periapsis
264.9553°
True anomaly
95.16927°
Mean anomaly
95.113°
Eccentric anomaly
95.14113°
Mean motion
3.85376 °/min
Orbital period
93.42 mins
BSTAR
0.00062836
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Other satellites on launch #91 in the year 2023 (2023-06-27 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 Z 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 | 2026-11-11 04:13:43.148Z | 106.856° ESE | 2026-11-11 04:15:43.148Z | 65.586° ENE | 18.026° | 2026-11-11 04:17:43.148Z | 27.331° NE |
| 4 mins | 2026-11-11 05:46:43.148Z | 231.349° WSW | 2026-11-11 05:47:43.148Z | 255.189° W | 21.56° | 2026-11-11 05:50:43.148Z | 316.934° NNW |
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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