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, 5.3 m
Radar Cross Section
25.344 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 SOYUZ MS-27
1 63520U 25072A 25258.38319791 .00010865 00000-0 19592-3 0 9994
2 63520 51.6329 220.0184 0004332 341.8913 18.1921 15.50310585 20201Epoch: 2025-09-15T09:11Z
TLE epoch observation values (Epoch: 2025-09-15T09:11:48.299Z)
Latitude
-0.00002°
Longitude
87.4785°
Altitude
413.763 km
Speed
7.666 km/s
True Right ascension
14h 40m 04s
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
13:30:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419.271 km
Perigee altitude
413.384 km
Semi-major axis
6,794.465 km
Eccentricity
0.00043
Inclination
51.6329°
RAAN
220.0184°
Arg. of periapsis
341.8913°
True anomaly
18.20761°
Mean anomaly
18.1921°
Eccentric anomaly
18.19985°
Mean motion
3.87534 °/min
Orbital period
92.89 mins
BSTAR
0.00019592
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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 | 2025-09-16 00:53:27.650Z | 258.367° W | 2025-09-16 00:55:27.650Z | 356.813° N | 37.4° | 2025-09-16 00:57:27.650Z | 41.086° NE |
| 4 mins | 2025-09-16 05:46:27.650Z | 347.461° N | 2025-09-16 05:47:27.650Z | 13.323° NNE | 22.695° | 2025-09-16 05:50:27.650Z | 81.984° E |
| 4 mins | 2025-09-16 07:23:27.650Z | 274.667° WNW | 2025-09-16 07:24:27.650Z | 236.085° WSW | 34.219° | 2025-09-16 07:27:27.650Z | 151.884° SSE |
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
Authenticating...
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