RASSVET-3 5, 68364
Orbit data source: Space-Track
RASSVET-3 5, 68364 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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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: 8 hours ago
TLE from 8 hours ago
0 RASSVET-3 5
1 68364U 26061E 26260.13727492 .00003612 00000-0 17424-3 0 9996
2 68364 82.2931 281.2937 0002115 70.7686 289.3776 15.18402535 27341Epoch: 2026-09-17T03:17Z
TLE epoch observation values (Epoch: 2026-09-17T03:17:40.553Z)
Latitude
-0.00001°
Longitude
-124.2041°
Altitude
513.264 km
Speed
7.607 km/s
True Right ascension
18h 45m 10s
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
04:06:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.105 km
Perigee altitude
506.193 km
Semi-major axis
6,885.786 km
Eccentricity
0.00021
Inclination
82.2931°
RAAN
281.2937°
Arg. of periapsis
70.7686°
True anomaly
289.35473°
Mean anomaly
289.3776°
Eccentric anomaly
289.36617°
Mean motion
3.79851 °/min
Orbital period
94.77 mins
BSTAR
0.00017424
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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 5 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-17 13:20:34.612Z | 358.235° N | 2026-09-17 13:23:34.612Z | 54.693° ENE | 67.589° | 2026-09-17 13:26:34.612Z | 163.505° S |
| 5 mins | 2026-09-18 01:34:34.612Z | 134.098° SE | 2026-09-18 01:36:34.612Z | 92.521° ESE | 24.239° | 2026-09-18 01:39:34.612Z | 36.982° NE |
| 4 mins | 2026-09-18 03:10:34.612Z | 253.217° W | 2026-09-18 03:12:34.612Z | 293.301° NW | 19.1° | 2026-09-18 03:14:34.612Z | 328.218° NNW |
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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