GONETS D1 9, 27060
Orbit data source: Space-Track
GONETS D1 9, 27060 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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27060 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 GONETS D1 9
1 27060U 01058F 26227.07129115 .00000025 00000-0 77303-4 0 9995
2 27060 82.5436 158.2300 0008200 164.0164 196.1187 12.63064187135264Epoch: 2026-08-15T01:42Z
TLE epoch observation values (Epoch: 2026-08-15T01:42:39.555Z)
Latitude
-0.00008°
Longitude
169.07774°
Altitude
1,419.189 km
Speed
7.148 km/s
True Right ascension
10h 32m 55s
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
02:12:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.028 km
Perigee altitude
1,401.259 km
Semi-major axis
7,785.78 km
Eccentricity
0.00082
Inclination
82.5436°
RAAN
158.23°
Arg. of periapsis
164.0164°
True anomaly
196.09264°
Mean anomaly
196.1187°
Eccentric anomaly
196.10567°
Mean motion
3.15929 °/min
Orbital period
113.95 mins
BSTAR
0.000077303
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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 9 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-08-15 18:56:00.910Z | 136.047° SSE | 2026-08-15 19:02:00.910Z | 83.621° E | 26.504° | 2026-08-15 19:08:00.910Z | 31.465° NE |
| 14 mins | 2026-08-15 20:50:00.910Z | 209.833° SW | 2026-08-15 20:56:00.910Z | 271.521° WNW | 39.213° | 2026-08-15 21:04:00.910Z | 358.259° N |
| 14 mins | 2026-08-16 06:51:00.910Z | 1.945° NNE | 2026-08-16 06:58:00.910Z | 92.589° ESE | 41.204° | 2026-08-16 07:05:00.910Z | 157.624° S |
| 11 mins | 2026-08-16 08:47:00.910Z | 321.037° NNW | 2026-08-16 08:52:00.910Z | 275.982° WNW | 23.83° | 2026-08-16 08:58:00.910Z | 227.125° WSW |
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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