PROGRESS MS-28, 60450 (Decayed)
Orbit data source: Space-Track
PROGRESS MS-28, 60450 was a payload satellite owned by RKKE (CIS) in LEO that was launched on Thu, 15 Aug 2024 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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60450 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Decayed Civil Spaceship
Bus & Motor
7K-TGM, 11D428A
Mass
7,427 kg wet, 4,325 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + Sphere + Cone + 2 Pan, 4.0 m
Radar Cross Section
19.615 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 PROGRESS MS-28
1 60450U 24145A 25056.53296170 .00025924 00000-0 46973-3 0 9996
2 60450 51.6375 140.0419 0005896 314.7988 171.5478 15.49435515497848Epoch: 2025-02-25T12:47Z
TLE epoch observation values (Epoch: 2025-02-25T12:47:27.890Z)
Latitude
39.28978°
Longitude
-67.55171°
Altitude
425.61 km
Speed
7.659 km/s
True Right ascension
18h 39m 47s
True Declination
39° 06' 47"
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
07:17:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.892 km
Perigee altitude
414.877 km
Semi-major axis
6,797.022 km
Eccentricity
0.00059
Inclination
51.6375°
RAAN
140.0419°
Arg. of periapsis
314.7988°
True anomaly
171.55772°
Mean anomaly
171.5478°
Eccentric anomaly
171.55276°
Mean motion
3.87316 °/min
Orbital period
92.95 mins
BSTAR
0.00046973
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Other satellites on launch #145 in the year 2024 (2024-08-15 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.PROGRESS MS-28 Visibility
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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. |
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| This satellite is decayed. |
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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