SL-4 R/B, 61044 (Decayed)
Orbit data source: Space-Track
SL-4 R/B, 61044 was space debris in LEO originally from a launch on Wed, 11 Sep 2024 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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61044 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Decayed spacecraft
Bus & Motor
BLOK-I, RD-0110
Mass
2,350 kg wet, 2,350 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 4.5 m
Radar Cross Section
21.560 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 SL-4 R/B
1 61044U 24162B 24257.35435400 .20508142 12653-4 36769-3 0 9991
2 61044 51.6564 237.6431 0005037 55.6763 97.7759 16.47424603 277Epoch: 2024-09-13T08:30Z
TLE epoch observation values (Epoch: 2024-09-13T08:30:16.185Z)
Latitude
20.528°
Longitude
-79.8777°
Altitude
146.94 km
Speed
7.821 km/s
True Right ascension
02h 42m 04s
True Declination
20° 24' 17"
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
22:43:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
149.939 km
Perigee altitude
143.366 km
Semi-major axis
6,524.789 km
Eccentricity
0.0005
Inclination
51.6564°
RAAN
237.6431°
Arg. of periapsis
55.6763°
True anomaly
97.83308°
Mean anomaly
97.7759°
Eccentric anomaly
97.80449°
Mean motion
4.11807 °/min
Orbital period
87.42 mins
BSTAR
0.00036769
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Other satellites on launch #162 in the year 2024 (2024-09-11 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.SL-4 R/B 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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