GONETS D1 3, 23789
Orbit data source: Space-Track
GONETS D1 3, 23789 is a payload satellite owned by Gonets (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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23789 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Non-operational Civil 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
1.798 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 GONETS D1 3
1 23789U 96009C 25259.68986329 .00000025 00000-0 80289-4 0 9995
2 23789 82.5787 134.4951 0005161 335.3242 24.7602 12.62675374363130Epoch: 2025-09-16T16:33Z
TLE epoch observation values (Epoch: 2025-09-16T16:33:24.188Z)
Latitude
0.00002°
Longitude
-109.73223°
Altitude
1,411 km
Speed
7.157 km/s
True Right ascension
08h 57m 58s
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
07:30:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.26 km
Perigee altitude
1,405.222 km
Semi-major axis
7,787.378 km
Eccentricity
0.00052
Inclination
82.5787°
RAAN
134.4951°
Arg. of periapsis
335.3242°
True anomaly
24.78498°
Mean anomaly
24.7602°
Eccentric anomaly
24.77259°
Mean motion
3.15832 °/min
Orbital period
113.98 mins
BSTAR
0.000080289
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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.GONETS D1 3 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-09-17 15:28:28.499Z | 149.59° SSE | 2025-09-17 15:35:28.499Z | 83.206° E | 32.66° | 2025-09-17 15:42:28.499Z | 22.867° NE |
| 14 mins | 2025-09-17 17:23:28.499Z | 220.748° SW | 2025-09-17 17:30:28.499Z | 291.915° WNW | 33.574° | 2025-09-17 17:37:28.499Z | 353.495° N |
| 7 mins | 2025-09-18 01:32:28.499Z | 41.401° NE | 2025-09-18 01:35:28.499Z | 65.175° ENE | 14.767° | 2025-09-18 01:39:28.499Z | 94.545° ESE |
| 15 mins | 2025-09-18 03:24:28.499Z | 355.386° N | 2025-09-18 03:31:28.499Z | 91.699° ESE | 44.6° | 2025-09-18 03:39:28.499Z | 169.747° S |
| 9 mins | 2025-09-18 05:21:28.499Z | 312.265° NW | 2025-09-18 05:25:28.499Z | 279.25° WNW | 18.26° | 2025-09-18 05:30:28.499Z | 241.069° WSW |
| 6 mins | 2025-09-18 14:22:28.499Z | 95.643° ESE | 2025-09-18 14:25:28.499Z | 72.72° E | 13.527° | 2025-09-18 14:28:28.499Z | 50.697° ENE |
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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