RASSVET-3 2, 68361
Orbit data source: Space-Track
RASSVET-3 2, 68361 is a payload satellite owned by Byuro 1440 (CIS) in LEO that was launched on Mon, 23 Mar 2026 UTC via a SOYUZ-2-1B 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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68361 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Byuro 1440
Mission
Operational Commercial Communications
Bus & Motor
RASSVET-2, Unknown motor
Mass
~370 kg wet, ~370 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 5.0 m
Radar Cross Section
6.123 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 RASSVET-3 2
1 68361U 26061B 26259.76545004 .00003686 00000-0 17561-3 0 9990
2 68361 82.2887 277.3147 0004392 135.9292 224.2292 15.18838445 27550Epoch: 2026-09-16T18:22Z
TLE epoch observation values (Epoch: 2026-09-16T18:22:14.883Z)
Latitude
-0.00006°
Longitude
6.04034°
Altitude
514.598 km
Speed
7.605 km/s
True Right ascension
18h 29m 15s
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
03:02:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.354 km
Perigee altitude
503.307 km
Semi-major axis
6,884.468 km
Eccentricity
0.00044
Inclination
82.2887°
RAAN
277.3147°
Arg. of periapsis
135.9292°
True anomaly
224.19411°
Mean anomaly
224.2292°
Eccentric anomaly
224.21165°
Mean motion
3.7996 °/min
Orbital period
94.75 mins
BSTAR
0.00017561
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Other satellites on launch #61 in the year 2026 (2026-03-23 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.RASSVET-3 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-17 12:19:26.143Z | 28.389° NE | 2026-09-17 12:22:26.143Z | 82.489° E | 18.94° | 2026-09-17 12:24:26.143Z | 117.003° SE |
| 4 mins | 2026-09-17 13:56:26.143Z | 297.89° NW | 2026-09-17 13:57:26.143Z | 274.06° WNW | 24.011° | 2026-09-17 14:00:26.143Z | 217.184° SW |
| 5 mins | 2026-09-18 02:08:26.143Z | 200.711° SSW | 2026-09-18 02:10:26.143Z | 300.77° NW | 68.687° | 2026-09-18 02:13:26.143Z | 1.784° NNE |
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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