GONETS D1 4, 24728
Orbit data source: Space-Track
GONETS D1 4, 24728 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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24728 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: 1 day ago
TLE from 1 day ago
0 GONETS D1 4
1 24728U 97006D 25259.89504011 .00000043 00000-0 17482-3 0 9998
2 24728 82.6032 50.5805 0008676 83.6117 276.5963 12.63914325318682Epoch: 2025-09-16T21:28Z
TLE epoch observation values (Epoch: 2025-09-16T21:28:51.465Z)
Latitude
-0.00001°
Longitude
92.28728°
Altitude
1,408.792 km
Speed
7.156 km/s
True Right ascension
03h 22m 19s
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
16:50:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,410.899 km
Perigee altitude
1,397.395 km
Semi-major axis
7,782.284 km
Eccentricity
0.00087
Inclination
82.6032°
RAAN
50.5805°
Arg. of periapsis
83.6117°
True anomaly
276.49753°
Mean anomaly
276.5963°
Eccentric anomaly
276.54691°
Mean motion
3.16142 °/min
Orbital period
113.87 mins
BSTAR
0.00017482
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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 4 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 | 2025-09-18 09:40:03.824Z | 147.132° SSE | 2025-09-18 09:47:03.824Z | 88.968° E | 30.042° | 2025-09-18 09:54:03.824Z | 25.951° NE |
| 14 mins | 2025-09-18 11:35:03.824Z | 215.444° SW | 2025-09-18 11:42:03.824Z | 287.84° WNW | 35.979° | 2025-09-18 11:49:03.824Z | 354.533° N |
| 5 mins | 2025-09-18 19:44:03.824Z | 44.213° NE | 2025-09-18 19:46:03.824Z | 59.337° ENE | 12.679° | 2025-09-18 19:49:03.824Z | 81.587° E |
| 14 mins | 2025-09-18 21:36:03.824Z | 358.761° N | 2025-09-18 21:43:03.824Z | 105.696° ESE | 43.21° | 2025-09-18 21:50:03.824Z | 164.16° S |
| 10 mins | 2025-09-18 23:32:03.824Z | 317.397° NNW | 2025-09-18 23:36:03.824Z | 284.099° WNW | 20.554° | 2025-09-18 23:42:03.824Z | 235.266° WSW |
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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