H-2A R/B, 45166 (Decayed)
Orbit data source: Space-Track
H-2A R/B, 45166 was space debris in LEO originally from a launch on Sun, 09 Feb 2020 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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45166 intel report (Beta)
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Edit Public Description
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 45166U 20009B 24113.86650667 .53867009 26681-5 20022-3 0 9993
2 45166 96.9487 155.0121 0009591 232.7556 210.3324 16.58268437235483Epoch: 2024-04-22T20:47Z
TLE epoch observation values (Epoch: 2024-04-22T20:47:46.176Z)
Latitude
80.2214°
Longitude
-53.0038°
Altitude
136.426 km
Speed
7.828 km/s
True Right ascension
07h 21m 21s
True Declination
80° 09' 29"
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
06:44:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
120.644 km
Perigee altitude
108.19 km
Semi-major axis
6,492.554 km
Eccentricity
0.00096
Inclination
96.9487°
RAAN
155.0121°
Arg. of periapsis
232.7556°
True anomaly
210.27695°
Mean anomaly
210.3324°
Eccentric anomaly
210.30467°
Mean motion
4.14877 °/min
Orbital period
86.77 mins
BSTAR
0.00020022
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Other satellites on launch #9 in the year 2020 (2020-02-09 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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