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: 17 hours ago
TLE from 17 hours ago
0 GONETS D1 8
1 27059U 01058E 25261.32449068 .00000014 00000-0 17354-4 0 9998
2 27059 82.5449 26.8408 0002868 133.4180 226.7150 12.61548319 92294Epoch: 2025-09-18T07:47Z
TLE epoch observation values (Epoch: 2025-09-18T07:47:15.994Z)
Latitude
0°
Longitude
-87.46356°
Altitude
1,420.821 km
Speed
7.15 km/s
True Right ascension
01h 47m 21s
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
17:58:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,416.118 km
Perigee altitude
1,411.648 km
Semi-major axis
7,792.02 km
Eccentricity
0.00029
Inclination
82.5449°
RAAN
26.8408°
Arg. of periapsis
133.418°
True anomaly
226.69108°
Mean anomaly
226.715°
Eccentric anomaly
226.70304°
Mean motion
3.1555 °/min
Orbital period
114.09 mins
BSTAR
0.000017354
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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 | 2025-09-19 08:36:45.916Z | 167.085° S | 2025-09-19 08:44:45.916Z | 84.283° E | 40.597° | 2025-09-19 08:51:45.916Z | 16.598° NNE |
| 12 mins | 2025-09-19 10:34:45.916Z | 242.046° WSW | 2025-09-19 10:39:45.916Z | 287.078° WNW | 25.528° | 2025-09-19 10:46:45.916Z | 346.529° N |
| 11 mins | 2025-09-19 18:40:45.916Z | 24.776° NE | 2025-09-19 18:45:45.916Z | 68.137° E | 21.839° | 2025-09-19 18:51:45.916Z | 116.08° SE |
| 14 mins | 2025-09-19 20:34:45.916Z | 346.368° N | 2025-09-19 20:41:45.916Z | 252.1° W | 43.287° | 2025-09-19 20:48:45.916Z | 186.067° 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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