FREGAT RB/CLUSTER 2, 26106
Orbit data source: Space-Track
FREGAT RB/CLUSTER 2, 26106 is a payload satellite owned by Starsem (CIS) in HEO that was launched on Mon, 20 Mar 2000 UTC via a SOYUZ-U-PVB launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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26106 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
AeMa Lanc
Mission
Commercial Technology
Bus & Motor
CLUSTER DUMMY, Unknown motor
Mass
3,382 kg wet, 1,191 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 1.0 m
Radar Cross Section
3.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 FREGAT RB/CLUSTER 2
1 26106U 00015A 25352.98521790 .00000101 00000-0 43533-4 0 9993
2 26106 65.1033 200.5209 5437067 273.9562 28.7465 4.61254216429894Epoch: 2025-12-18T23:38Z
TLE epoch observation values (Epoch: 2025-12-18T23:38:42.826Z)
Latitude
-0.00014°
Longitude
118.01581°
Altitude
3,984.99 km
Speed
7.127 km/s
True Right ascension
13h 22m 06s
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
12:22:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
17,152.882 km
Perigee altitude
577.23 km
Semi-major axis
15,243.193 km
Eccentricity
0.54371
Inclination
65.1033°
RAAN
200.5209°
Arg. of periapsis
273.9562°
True anomaly
86.19329°
Mean anomaly
28.7465°
Eccentric anomaly
53.92513°
Mean motion
1.15327 °/min
Orbital period
312.16 mins
BSTAR
0.000043533
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Other satellites on launch #15 in the year 2000 (2000-03-20 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.FREGAT RB/CLUSTER 2 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. |
|---|---|---|---|---|---|---|---|
| 186 mins | 2025-12-21 14:04:28.778Z | 176.109° S | 2025-12-21 14:37:28.778Z | 94.839° ESE | 43.151° | 2025-12-21 17:10:28.778Z | 41.403° NE |
| 231 mins | 2025-12-21 19:40:28.778Z | 281.365° WNW | 2025-12-21 22:28:28.778Z | 43.82° NE | 41.892° | 2025-12-21 23:31:28.778Z | 124.463° SE |
| 155 mins | 2025-12-22 02:07:28.778Z | 331.996° NNW | 2025-12-22 03:54:28.778Z | 296.948° NW | 30.16° | 2025-12-22 04:42:28.778Z | 240.155° WSW |
| 117 mins | 2025-12-22 11:09:28.778Z | 92.031° ESE | 2025-12-22 11:48:28.778Z | 52.921° ENE | 21.953° | 2025-12-22 13:06:28.778Z | 25.068° NE |
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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