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 25307.95706213 .00000044 00000-0 18976-3 0 9999
2 27059 82.5443 356.9932 0002864 62.3601 297.7780 12.61550049 98174Epoch: 2025-11-03T22:58Z
TLE epoch observation values (Epoch: 2025-11-03T22:58:10.168Z)
Latitude
-0°
Longitude
-31.00016°
Altitude
1,418.241 km
Speed
7.152 km/s
True Right ascension
23h 47m 58s
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
02:15:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,416.108 km
Perigee altitude
1,411.645 km
Semi-major axis
7,792.013 km
Eccentricity
0.00029
Inclination
82.5443°
RAAN
356.9932°
Arg. of periapsis
62.3601°
True anomaly
297.74896°
Mean anomaly
297.778°
Eccentric anomaly
297.76348°
Mean motion
3.1555 °/min
Orbital period
114.09 mins
BSTAR
0.00018976
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-11-04 14:49:26.807Z | 2.86° NNE | 2025-11-04 14:55:26.807Z | 68.563° E | 41.18° | 2025-11-04 15:03:26.807Z | 157.725° S |
| 11 mins | 2025-11-04 16:45:26.807Z | 320.362° NNW | 2025-11-04 16:50:26.807Z | 274.65° WNW | 24.109° | 2025-11-04 16:56:26.807Z | 226.448° WSW |
| 14 mins | 2025-11-05 03:37:26.807Z | 166.543° S | 2025-11-05 03:43:26.807Z | 104.531° ESE | 41.339° | 2025-11-05 03:51:26.807Z | 15.04° NNE |
| 11 mins | 2025-11-05 05:34:26.807Z | 245.658° WSW | 2025-11-05 05:39:26.807Z | 291.281° WNW | 24.507° | 2025-11-05 05:45:26.807Z | 342.665° 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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