H-2A R/B, 57804 (Decayed)
Orbit data source: Space-Track
H-2A R/B, 57804 was space debris in HEO originally from a launch on Wed, 06 Sep 2023 UTC launched from the Tanegashima Space Center (TNSTA). 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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57804 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
MHI Tobishima
Mission
Decayed spacecraft
Bus & Motor
H-2A STAGE 2, Unknown motor
Mass
4,000 kg wet, 4,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 4.6 m
Radar Cross Section
35.186 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 H-2A R/B
1 57804U 23137E 25003.00000000 .00211024 65637-6 18424-1 0 9993
2 57804 29.7777 323.9967 8550846 328.0463 109.6870 0.90647478 3308Epoch: 2025-01-03T00:00Z
TLE epoch observation values (Epoch: 2025-01-03T00:00:00.000Z)
Latitude
19.92574°
Longitude
1.90746°
Altitude
68,709.385 km
Speed
1.334 km/s
True Right ascension
06h 59m 06s
True Declination
19° 54' 55"
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
21:38:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
77,292.136 km
Perigee altitude
158.013 km
Semi-major axis
45,103.211 km
Eccentricity
0.85508
Inclination
29.7777°
RAAN
323.9967°
Arg. of periapsis
328.0463°
True anomaly
168.60502°
Mean anomaly
109.687°
Eccentric anomaly
140.71087°
Mean motion
0.22659 °/min
Orbital period
1,588.8 mins
BSTAR
0.018424
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Other satellites on launch #137 in the year 2023 (2023-09-06 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.H-2A 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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