GONETS D1 8, 27059
Orbit data source: Space-Track
GONETS D1 8, 27059 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Fri, 28 Dec 2001 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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27059 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: 3 hours ago
TLE from 3 hours ago
0 GONETS D1 8
1 27059U 01058E 25355.54124744 -.00000048 00000-0 -32807-3 0 9995
2 27059 82.5418 326.5155 0001277 326.4465 33.6544 12.61551215104174Epoch: 2025-12-21T12:59Z
TLE epoch observation values (Epoch: 2025-12-21T12:59:23.778Z)
Latitude
-0.00009°
Longitude
41.3142°
Altitude
1,418.447 km
Speed
7.152 km/s
True Right ascension
21h 46m 03s
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
14:55:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.866 km
Perigee altitude
1,412.876 km
Semi-major axis
7,792.008 km
Eccentricity
0.00013
Inclination
82.5418°
RAAN
326.5155°
Arg. of periapsis
326.4465°
True anomaly
33.66251°
Mean anomaly
33.6544°
Eccentric anomaly
33.65846°
Mean motion
3.15551 °/min
Orbital period
114.09 mins
BSTAR
-0.00032807
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Other satellites on launch #58 in the year 2001 (2001-12-28 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 8 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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2025-12-21 22:35:12.752Z | 171.198° S | 2025-12-21 22:43:12.752Z | 86.14° E | 42.266° | 2025-12-21 22:51:12.752Z | 13.495° NNE |
| 12 mins | 2025-12-22 00:33:12.752Z | 244.306° WSW | 2025-12-22 00:39:12.752Z | 297.036° NW | 23.416° | 2025-12-22 00:45:12.752Z | 344.636° N |
| 11 mins | 2025-12-22 08:39:12.752Z | 22.523° NE | 2025-12-22 08:44:12.752Z | 66.824° ENE | 23.893° | 2025-12-22 08:50:12.752Z | 118.172° SE |
| 15 mins | 2025-12-22 10:33:12.752Z | 344.257° N | 2025-12-22 10:40:12.752Z | 260.534° W | 41.973° | 2025-12-22 10:48:12.752Z | 189.059° SSW |
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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