RASSVET-3 10, 68369
Orbit data source: Space-Track
RASSVET-3 10, 68369 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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68369 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: 7 hours ago
TLE from 7 hours ago
0 RASSVET-3 10
1 68369U 26061K 26261.15117894 .00001900 00000-0 89662-4 0 9995
2 68369 82.2822 271.6300 0004217 122.8868 237.2772 15.18889813 28031Epoch: 2026-09-18T03:37Z
TLE epoch observation values (Epoch: 2026-09-18T03:37:41.860Z)
Latitude
-0.00001°
Longitude
-139.8726°
Altitude
513.846 km
Speed
7.606 km/s
True Right ascension
18h 06m 31s
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
02:58:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.079 km
Perigee altitude
503.272 km
Semi-major axis
6,884.313 km
Eccentricity
0.00042
Inclination
82.2822°
RAAN
271.63°
Arg. of periapsis
122.8868°
True anomaly
237.23656°
Mean anomaly
237.2772°
Eccentric anomaly
237.25688°
Mean motion
3.79973 °/min
Orbital period
94.74 mins
BSTAR
0.000089662
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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 10 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 | 2026-09-18 12:05:22.214Z | 19.246° NNE | 2026-09-18 12:08:22.214Z | 74.723° E | 25.784° | 2026-09-18 12:11:22.214Z | 131.864° SE |
| 4 mins | 2026-09-18 13:42:22.214Z | 299.169° NW | 2026-09-18 13:43:22.214Z | 280.543° WNW | 17.492° | 2026-09-18 13:46:22.214Z | 228.352° WSW |
| 5 mins | 2026-09-19 01:54:22.214Z | 213.885° SW | 2026-09-19 01:56:22.214Z | 269.687° W | 48.159° | 2026-09-19 01:59:22.214Z | 351.958° 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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