H-2A R/B, 61440
Orbit data source: Space-Track
H-2A R/B, 61440 is space debris in SSO originally from a launch on Thu, 26 Sep 2024 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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61440 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 H-2A R/B
1 61440U 24176B 25243.29186821 .00043736 00000-0 90104-3 0 9998
2 61440 97.2506 13.2761 0011848 272.5541 87.4352 15.45717468 52042
Epoch: 2025-08-31T07:00Z
TLE epoch observation values (Epoch: 2025-08-31T07:00:17.413Z)
Latitude
-0.00002°
Longitude
-71.51036°
Altitude
432.049 km
Speed
7.653 km/s
True Right ascension
00h 53m 06s
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
05:06:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.257 km
Perigee altitude
418.134 km
Semi-major axis
6,804.333 km
Eccentricity
0.00118
Inclination
97.2506°
RAAN
13.2761°
Arg. of periapsis
272.5541°
True anomaly
87.57084°
Mean anomaly
87.4352°
Eccentric anomaly
87.50302°
Mean motion
3.86692 °/min
Orbital period
93.1 mins
BSTAR
0.00090104
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Other satellites on launch #176 in the year 2024 (2024-09-26 UTC)
H-2A R/B Visibility forecast
Observer location: undefined°, undefined°
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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5 mins | 2025-08-31 21:32:56.580Z | 15.13° NNE | 2025-08-31 21:35:56.580Z | 169.467° S | 41.826° | 2025-08-31 21:37:56.580Z | 187.925° SSW |
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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