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: 14 hours ago
TLE from 14 hours ago
0 SOYUZ MS-27
1 63520U 25072A 25334.54411181 .00007982 00000-0 15180-3 0 9998
2 63520 51.6312 202.8529 0003690 187.0517 173.0420 15.49206888 20203Epoch: 2025-11-30T13:03Z
TLE epoch observation values (Epoch: 2025-11-30T13:03:31.260Z)
Latitude
-0.00003°
Longitude
-62.68382°
Altitude
422.275 km
Speed
7.658 km/s
True Right ascension
13h 31m 24s
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
00:22:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.063 km
Perigee altitude
417.046 km
Semi-major axis
6,797.691 km
Eccentricity
0.00037
Inclination
51.6312°
RAAN
202.8529°
Arg. of periapsis
187.0517°
True anomaly
173.04712°
Mean anomaly
173.042°
Eccentric anomaly
173.04456°
Mean motion
3.87259 °/min
Orbital period
92.96 mins
BSTAR
0.0001518
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-01 17:05:31.751Z | 172.675° S | 2025-12-01 17:07:31.751Z | 127.468° SE | 19.267° | 2025-12-01 17:09:31.751Z | 86.687° E |
| 4 mins | 2025-12-01 18:42:31.751Z | 272.39° WNW | 2025-12-01 18:43:31.751Z | 304.693° NW | 33.082° | 2025-12-01 18:46:31.751Z | 37.969° NE |
| 4 mins | 2025-12-01 23:35:31.751Z | 343.692° N | 2025-12-01 23:36:31.751Z | 10.954° NNE | 25.621° | 2025-12-01 23:39:31.751Z | 87.586° E |
| 4 mins | 2025-12-02 01:12:31.751Z | 267.273° W | 2025-12-02 01:13:31.751Z | 235.318° WSW | 28.224° | 2025-12-02 01:16:31.751Z | 160.964° S |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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