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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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: 10 hours ago
TLE from 10 hours ago
0 GONETS D1 3
1 23789U 96009C 26140.00481505 .00000006 00000-0 -23933-4 0 9990
2 23789 82.5788 337.8478 0006128 123.0237 237.1443 12.62685193394096Epoch: 2026-05-20T00:06Z
TLE epoch observation values (Epoch: 2026-05-20T00:06:56.020Z)
Latitude
-0.00009°
Longitude
98.44378°
Altitude
1,417.203 km
Speed
7.151 km/s
True Right ascension
22h 31m 23s
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
19:26:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.973 km
Perigee altitude
1,404.429 km
Semi-major axis
7,787.338 km
Eccentricity
0.00061
Inclination
82.5788°
RAAN
337.8478°
Arg. of periapsis
123.0237°
True anomaly
237.08534°
Mean anomaly
237.1443°
Eccentric anomaly
237.11482°
Mean motion
3.15835 °/min
Orbital period
113.98 mins
BSTAR
-0.000023933
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2026-05-20 13:30:36.691Z | 171.095° S | 2026-05-20 13:38:36.691Z | 79.252° E | 42.211° | 2026-05-20 13:45:36.691Z | 14.372° NNE |
| 11 mins | 2026-05-20 15:28:36.691Z | 245.986° WSW | 2026-05-20 15:33:36.691Z | 289.298° WNW | 23.35° | 2026-05-20 15:39:36.691Z | 340.895° N |
| 11 mins | 2026-05-20 23:33:36.691Z | 21.12° NNE | 2026-05-20 23:38:36.691Z | 64.139° ENE | 23.554° | 2026-05-20 23:44:36.691Z | 116.717° SE |
| 15 mins | 2026-05-21 01:27:36.691Z | 344.749° N | 2026-05-21 01:34:36.691Z | 265.522° W | 42.117° | 2026-05-21 01:42:36.691Z | 188.917° 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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