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: 7 hours ago
TLE from 7 hours ago
0 GONETS D1 8
1 27059U 01058E 25308.59151836 .00000032 00000-0 12091-3 0 9994
2 27059 82.5442 356.5869 0002848 61.4353 298.7024 12.61550050 98257Epoch: 2025-11-04T14:11Z
TLE epoch observation values (Epoch: 2025-11-04T14:11:47.186Z)
Latitude
-0.00001°
Longitude
99.56395°
Altitude
1,418.215 km
Speed
7.152 km/s
True Right ascension
23h 46m 20s
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
17:16:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,416.095 km
Perigee altitude
1,411.657 km
Semi-major axis
7,792.013 km
Eccentricity
0.00028
Inclination
82.5442°
RAAN
356.5869°
Arg. of periapsis
61.4353°
True anomaly
298.67377°
Mean anomaly
298.7024°
Eccentric anomaly
298.68809°
Mean motion
3.1555 °/min
Orbital period
114.09 mins
BSTAR
0.00012091
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-11-05 03:36:02.444Z | 169.137° S | 2025-11-05 03:44:02.444Z | 84.865° E | 41.459° | 2025-11-05 03:51:02.444Z | 15.681° NNE |
| 12 mins | 2025-11-05 05:34:02.444Z | 243.237° WSW | 2025-11-05 05:39:02.444Z | 286.716° WNW | 24.431° | 2025-11-05 05:46:02.444Z | 345.634° N |
| 11 mins | 2025-11-05 13:40:02.444Z | 23.774° NE | 2025-11-05 13:45:02.444Z | 67.705° E | 22.863° | 2025-11-05 13:51:02.444Z | 117.192° SE |
| 14 mins | 2025-11-05 15:34:02.444Z | 345.27° N | 2025-11-05 15:41:02.444Z | 256.176° W | 42.67° | 2025-11-05 15:48:02.444Z | 188.259° 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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