SOYUZ MS-27, 63520
Orbit data source: Space-Track
SOYUZ MS-27, 63520 is a payload satellite owned by RKKE (CIS) in LEO that was launched on Tue, 08 Apr 2025 UTC via a SOYUZ-2-1A 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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63520 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
RKKE
Mission
Operational Civil Spaceship
Bus & Motor
7K-S A48, SA
Mass
7,152 kg wet, 2,900 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + Cone + Sphere + 2 Pan, 14.5 m
Radar Cross Section
25.344 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 SOYUZ MS-27
1 63520U 25072A 25289.78310296 .00013924 00000-0 25892-3 0 9992
2 63520 51.6332 64.4492 0004220 298.8409 61.2156 15.49164717 20205Epoch: 2025-10-16T18:47Z
TLE epoch observation values (Epoch: 2025-10-16T18:47:40.095Z)
Latitude
-0°
Longitude
116.99426°
Altitude
418.528 km
Speed
7.662 km/s
True Right ascension
04h 17m 47s
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
22:43:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.546 km
Perigee altitude
416.808 km
Semi-major axis
6,797.814 km
Eccentricity
0.00042
Inclination
51.6332°
RAAN
64.4492°
Arg. of periapsis
298.8409°
True anomaly
61.25799°
Mean anomaly
61.2156°
Eccentric anomaly
61.2368°
Mean motion
3.87248 °/min
Orbital period
92.96 mins
BSTAR
0.00025892
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Other satellites on launch #72 in the year 2025 (2025-04-08 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.SOYUZ MS-27 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 | 2025-10-17 12:00:46.552Z | 231.064° WSW | 2025-10-17 12:03:46.552Z | 59.301° ENE | 44.297° | 2025-10-17 12:06:46.552Z | 53.066° ENE |
| 5 mins | 2025-10-17 18:31:46.552Z | 302.344° NW | 2025-10-17 18:33:46.552Z | 171.129° S | 43.718° | 2025-10-17 18:36:46.552Z | 132.788° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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