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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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: 16 hours ago
TLE from 16 hours ago
0 GONETS D1 4
1 24728U 97006D 26127.85879235 .00000035 00000-0 13469-3 0 9994
2 24728 82.6029 262.0013 0006764 270.0264 90.0053 12.63922219348111Epoch: 2026-05-07T20:36Z
TLE epoch observation values (Epoch: 2026-05-07T20:36:39.659Z)
Latitude
0°
Longitude
87.13716°
Altitude
1,409.534 km
Speed
7.156 km/s
True Right ascension
17h 28m 00s
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
20:51:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,409.379 km
Perigee altitude
1,398.851 km
Semi-major axis
7,782.252 km
Eccentricity
0.00068
Inclination
82.6029°
RAAN
262.0013°
Arg. of periapsis
270.0264°
True anomaly
90.08281°
Mean anomaly
90.0053°
Eccentric anomaly
90.04405°
Mean motion
3.16144 °/min
Orbital period
113.87 mins
BSTAR
0.00013469
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2026-05-08 20:01:10.275Z | 5.212° NNE | 2026-05-08 20:08:10.275Z | 74.265° E | 36.852° | 2026-05-08 20:16:10.275Z | 149.189° SSE |
| 12 mins | 2026-05-08 21:57:10.275Z | 328.504° NNW | 2026-05-08 22:03:10.275Z | 269.667° W | 29.228° | 2026-05-08 22:09:10.275Z | 217.597° SW |
| 13 mins | 2026-05-09 08:49:10.275Z | 153.677° SSE | 2026-05-09 08:55:10.275Z | 86.356° E | 36.683° | 2026-05-09 09:02:10.275Z | 20.318° NNE |
| 13 mins | 2026-05-09 10:44:10.275Z | 231.16° WSW | 2026-05-09 10:50:10.275Z | 289.535° WNW | 29.77° | 2026-05-09 10:57:10.275Z | 350.297° 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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