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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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: 23 hours ago
TLE from 23 hours ago
0 COSMOS 2328
1 23790U 96009D 26267.47986674 .00000032 00000-0 11843-3 0 9994
2 23790 82.5729 256.1692 0007456 183.3695 176.7348 12.62605531410006Epoch: 2026-09-24T11:31Z
TLE epoch observation values (Epoch: 2026-09-24T11:31:00.486Z)
Latitude
0.00006°
Longitude
80.10114°
Altitude
1,420.739 km
Speed
7.148 km/s
True Right ascension
17h 04m 40s
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
03:52:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,415.335 km
Perigee altitude
1,403.722 km
Semi-major axis
7,787.666 km
Eccentricity
0.00075
Inclination
82.5729°
RAAN
256.1692°
Arg. of periapsis
183.3695°
True anomaly
176.73966°
Mean anomaly
176.7348°
Eccentric anomaly
176.73723°
Mean motion
3.15815 °/min
Orbital period
113.99 mins
BSTAR
0.00011843
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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 | 2026-09-25 10:56:02.977Z | 355.736° N | 2026-09-25 11:04:02.977Z | 59.15° ENE | 72.321° | 2026-09-25 11:12:02.977Z | 165.327° S |
| 10 mins | 2026-09-25 12:54:02.977Z | 316.953° NNW | 2026-09-25 12:58:02.977Z | 284.064° WNW | 21.483° | 2026-09-25 13:04:02.977Z | 236.009° WSW |
| 4 mins | 2026-09-25 21:57:02.977Z | 84.003° E | 2026-09-25 21:58:02.977Z | 76.596° E | 12.256° | 2026-09-25 22:01:02.977Z | 54.919° ENE |
| 15 mins | 2026-09-25 23:45:02.977Z | 175.249° S | 2026-09-25 23:52:02.977Z | 72.943° E | 73.315° | 2026-09-26 00:00:02.977Z | 11.217° NNE |
| 10 mins | 2026-09-26 01:43:02.977Z | 255.312° W | 2026-09-26 01:47:02.977Z | 289.26° WNW | 22.501° | 2026-09-26 01:53:02.977Z | 338.865° N |
| 12 mins | 2026-09-26 09:47:02.977Z | 18.401° NNE | 2026-09-26 09:53:02.977Z | 74.034° E | 29.505° | 2026-09-26 09:59:02.977Z | 124.882° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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