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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 GONETS D1 4
1 24728U 97006D 26308.02307904 .00000031 00000-0 10992-3 0 9997
2 24728 82.6024 147.1355 0007139 218.6170 141.4412 12.63924751370870Epoch: 2026-11-04T00:33Z
TLE epoch observation values (Epoch: 2026-11-04T00:33:14.029Z)
Latitude
-0.00002°
Longitude
95.54969°
Altitude
1,413.868 km
Speed
7.152 km/s
True Right ascension
09h 48m 32s
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
11:10:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,409.66 km
Perigee altitude
1,398.548 km
Semi-major axis
7,782.241 km
Eccentricity
0.00071
Inclination
82.6024°
RAAN
147.1355°
Arg. of periapsis
218.617°
True anomaly
141.49216°
Mean anomaly
141.4412°
Eccentric anomaly
141.46668°
Mean motion
3.16145 °/min
Orbital period
113.87 mins
BSTAR
0.00010992
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-11-04 15:53:53.467Z | 248.916° W | 2026-11-04 15:59:53.467Z | 297.625° NW | 21.842° | 2026-11-04 16:04:53.467Z | 337.668° N |
| 12 mins | 2026-11-04 23:58:53.467Z | 20.052° NNE | 2026-11-05 00:03:53.467Z | 66.006° ENE | 29.975° | 2026-11-05 00:10:53.467Z | 127.006° SE |
| 14 mins | 2026-11-05 01:52:53.467Z | 341.051° N | 2026-11-05 01:59:53.467Z | 258.084° W | 55.5° | 2026-11-05 02:06:53.467Z | 195.615° SSW |
| 12 mins | 2026-11-05 12:45:53.467Z | 134.589° SE | 2026-11-05 12:51:53.467Z | 81.657° E | 29.328° | 2026-11-05 12:57:53.467Z | 30.993° NE |
| 15 mins | 2026-11-05 14:38:53.467Z | 206.855° SW | 2026-11-05 14:45:53.467Z | 277.486° WNW | 56.257° | 2026-11-05 14:53:53.467Z | 359.043° 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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