COSMOS 2328, 23790
Orbit data source: Space-Track
COSMOS 2328, 23790 is a payload satellite owned by VKS (CIS) in LEO that was launched on Mon, 19 Feb 1996 UTC via a TSIKLON-3 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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23790 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Non-operational Defense Communications
Bus & Motor
STRELA-3, Unknown motor
Mass
225 kg wet, 225 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Ant, 3.5 m
Radar Cross Section
1.583 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 COSMOS 2328
1 23790U 96009D 25302.91619157 .00000043 00000-0 17866-3 0 9994
2 23790 82.5733 106.6118 0007295 213.9580 146.1045 12.62596257368413Epoch: 2025-10-29T21:59Z
TLE epoch observation values (Epoch: 2025-10-29T21:59:18.951Z)
Latitude
-0.00004°
Longitude
98.30036°
Altitude
1,419.696 km
Speed
7.149 km/s
True Right ascension
07h 06m 26s
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
04:30:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,415.248 km
Perigee altitude
1,403.886 km
Semi-major axis
7,787.704 km
Eccentricity
0.00073
Inclination
82.5733°
RAAN
106.6118°
Arg. of periapsis
213.958°
True anomaly
146.15108°
Mean anomaly
146.1045°
Eccentric anomaly
146.1278°
Mean motion
3.15812 °/min
Orbital period
113.99 mins
BSTAR
0.00017866
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Other satellites on launch #9 in the year 1996 (1996-02-19 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.COSMOS 2328 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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2025-10-30 11:22:37.136Z | 172.007° S | 2025-10-30 11:30:37.136Z | 96.677° ESE | 42.48° | 2025-10-30 11:38:37.136Z | 13.541° NNE |
| 11 mins | 2025-10-30 13:21:37.136Z | 249.607° W | 2025-10-30 13:26:37.136Z | 295.093° NW | 23.251° | 2025-10-30 13:32:37.136Z | 343.547° N |
| 11 mins | 2025-10-30 21:26:37.136Z | 23.75° NE | 2025-10-30 21:31:37.136Z | 69.132° E | 23.879° | 2025-10-30 21:37:37.136Z | 119.437° SE |
| 14 mins | 2025-10-30 23:20:37.136Z | 343.703° N | 2025-10-30 23:26:37.136Z | 285.12° WNW | 41.696° | 2025-10-30 23:34:37.136Z | 190.119° 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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