GRAVITY-1 R/B, 58761 (Decayed)
Orbit data source: Space-Track
GRAVITY-1 R/B, 58761 was space debris in LEO originally from a launch on Thu, 11 Jan 2024 UTC launched from the Yellow Sea Launch Area, China (YSLA). 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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58761 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
1,000 kg wet, 1,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.3 m
Radar Cross Section
6.920 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 GRAVITY-1 R/B
1 58761U 24009D 24181.82249840 .11988195 12669-4 11278-3 0 9997
2 58761 49.8264 331.8718 0009603 332.7203 180.0023 16.50665787 26992Epoch: 2024-06-29T19:44Z
TLE epoch observation values (Epoch: 2024-06-29T19:44:23.861Z)
Latitude
20.55283°
Longitude
-80.9515°
Altitude
143.999 km
Speed
7.819 km/s
True Right ascension
08h 54m 06s
True Declination
20° 25' 46"
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
14:27:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
144.685 km
Perigee altitude
132.169 km
Semi-major axis
6,516.564 km
Eccentricity
0.00096
Inclination
49.8264°
RAAN
331.8718°
Arg. of periapsis
332.7203°
True anomaly
180.0023°
Mean anomaly
180.0023°
Eccentric anomaly
180.0023°
Mean motion
4.12587 °/min
Orbital period
87.25 mins
BSTAR
0.00011278
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Other satellites on launch #9 in the year 2024 (2024-01-11 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.GRAVITY-1 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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