GONETS D1 6, 24730
Orbit data source: Space-Track
GONETS D1 6, 24730 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Fri, 14 Feb 1997 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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24730 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: 12 hours ago
TLE from 12 hours ago
0 GONETS D1 6
1 24730U 97006F 25307.96717697 .00000016 00000-0 28479-4 0 9998
2 24730 82.6111 40.2762 0003661 105.7134 254.4362 12.62490905323254Epoch: 2025-11-03T23:12Z
TLE epoch observation values (Epoch: 2025-11-03T23:12:44.090Z)
Latitude
0.00006°
Longitude
8.63154°
Altitude
1,416.177 km
Speed
7.152 km/s
True Right ascension
02h 41m 06s
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
06:55:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.85 km
Perigee altitude
1,407.148 km
Semi-major axis
7,788.136 km
Eccentricity
0.00037
Inclination
82.6111°
RAAN
40.2762°
Arg. of periapsis
105.7134°
True anomaly
254.39579°
Mean anomaly
254.4362°
Eccentric anomaly
254.416°
Mean motion
3.15786 °/min
Orbital period
114 mins
BSTAR
0.000028479
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Other satellites on launch #6 in the year 1997 (1997-02-14 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 6 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 | 2025-11-04 16:55:49.442Z | 10.169° NNE | 2025-11-04 17:02:49.442Z | 68.683° E | 28.194° | 2025-11-04 17:09:49.442Z | 130.396° SE |
| 14 mins | 2025-11-04 18:51:49.442Z | 339.087° N | 2025-11-04 18:57:49.442Z | 280.233° WNW | 37.994° | 2025-11-04 19:05:49.442Z | 198.386° SSW |
| 12 mins | 2025-11-05 05:45:49.442Z | 136.074° SSE | 2025-11-05 05:51:49.442Z | 78.059° E | 27.875° | 2025-11-05 05:57:49.442Z | 28.333° NE |
| 14 mins | 2025-11-05 07:39:49.442Z | 214.005° SW | 2025-11-05 07:45:49.442Z | 281.3° WNW | 38.014° | 2025-11-05 07:53:49.442Z | 357.962° N |
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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