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: 12 hours ago
TLE from 12 hours ago
0 GONETS D1 4
1 24728U 97006D 25307.94439779 .00000019 00000-0 44749-4 0 9996
2 24728 82.6090 19.9457 0007051 339.7751 20.3061 12.63916016324751Epoch: 2025-11-03T22:39Z
TLE epoch observation values (Epoch: 2025-11-03T22:39:55.969Z)
Latitude
0.00002°
Longitude
-3.47601°
Altitude
1,404.407 km
Speed
7.16 km/s
True Right ascension
01h 19m 46s
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
06:59:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,409.627 km
Perigee altitude
1,398.653 km
Semi-major axis
7,782.277 km
Eccentricity
0.00071
Inclination
82.609°
RAAN
19.9457°
Arg. of periapsis
339.7751°
True anomaly
20.33416°
Mean anomaly
20.3061°
Eccentric anomaly
20.32013°
Mean motion
3.16143 °/min
Orbital period
113.87 mins
BSTAR
0.000044749
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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 | 2025-11-04 16:23:07.671Z | 1.359° NNE | 2025-11-04 16:30:07.671Z | 91.396° ESE | 41.687° | 2025-11-04 16:37:07.671Z | 158.595° S |
| 11 mins | 2025-11-04 18:19:07.671Z | 320.519° NNW | 2025-11-04 18:24:07.671Z | 275.841° WNW | 23.405° | 2025-11-04 18:30:07.671Z | 227.844° WSW |
| 14 mins | 2025-11-05 05:10:07.671Z | 167.033° S | 2025-11-05 05:16:07.671Z | 99.823° ESE | 41.722° | 2025-11-05 05:24:07.671Z | 14.377° NNE |
| 12 mins | 2025-11-05 07:06:07.671Z | 242.364° WSW | 2025-11-05 07:12:07.671Z | 295.451° NW | 23.985° | 2025-11-05 07:18:07.671Z | 344.341° 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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