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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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: 18 hours ago
TLE from 18 hours ago
0 GONETS D1 8
1 27059U 01058E 26096.25725539 .00000057 00000-0 26463-3 0 9994
2 27059 82.5371 258.8039 0002821 67.0523 293.0864 12.61555787117505Epoch: 2026-04-06T06:10Z
TLE epoch observation values (Epoch: 2026-04-06T06:10:26.865Z)
Latitude
-0.00013°
Longitude
-28.35898°
Altitude
1,418.395 km
Speed
7.152 km/s
True Right ascension
17h 15m 12s
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
06:36:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,416.051 km
Perigee altitude
1,411.655 km
Semi-major axis
7,791.99 km
Eccentricity
0.00028
Inclination
82.5371°
RAAN
258.8039°
Arg. of periapsis
67.0523°
True anomaly
293.05666°
Mean anomaly
293.0864°
Eccentric anomaly
293.07153°
Mean motion
3.15552 °/min
Orbital period
114.09 mins
BSTAR
0.00026463
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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 | 2026-04-07 10:48:27.028Z | 162.973° S | 2026-04-07 10:56:27.028Z | 81.469° E | 38.649° | 2026-04-07 11:03:27.028Z | 18.142° NNE |
| 13 mins | 2026-04-07 12:45:27.028Z | 234.442° WSW | 2026-04-07 12:51:27.028Z | 288.97° WNW | 27.637° | 2026-04-07 12:58:27.028Z | 348.707° N |
| 10 mins | 2026-04-07 20:52:27.028Z | 27.257° NE | 2026-04-07 20:57:27.028Z | 69.693° E | 19.908° | 2026-04-07 21:02:27.028Z | 109.087° ESE |
| 14 mins | 2026-04-07 22:46:27.028Z | 348.517° N | 2026-04-07 22:53:27.028Z | 233.237° WSW | 44.109° | 2026-04-07 23:00:27.028Z | 181.731° 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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