H-2A R/B, 40268

Orbit data source: Space-Track

H-2A R/B, 40268 is space debris in HEO originally from a launch on Tue, 07 Oct 2014 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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Identifier
40268, 2014-060B
Orbit
HEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
MHI Tobishima
Mission
Spacecraft
Bus & Motor
H-2A STAGE 2, Unknown motor
Mass
4,000 kg wet, 4,000 kg dry
Launch date (UTC)
2014-10-07 (12 years ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 5.0 m
Radar Cross Section
35.186 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 H-2A R/B
1 40268U 14060B   26297.03711593  .00010823  00000-0  70237-3 0  9992
2 40268  22.3508 207.4409 6560235 255.7822  28.0355  3.27358221118080
Epoch: 2026-10-24T00:53Z
TLE epoch observation values (Epoch: 2026-10-24T00:53:26.816Z)
Latitude
0.00029°
Longitude
161.6555°
Altitude
6,659.2 km
Speed
6.351 km/s
True Right ascension
13h 49m 51s
True Declination
0° 00' 01"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
10:52:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
25,357.558 km
Perigee altitude
213.758 km
Semi-major axis
19,163.795 km
Eccentricity
0.65602
Inclination
22.3508°
RAAN
207.4409°
Arg. of periapsis
255.7822°
True anomaly
104.39439°
Mean anomaly
28.0355°
Eccentric anomaly
60.86814°
Mean motion
0.81813 °/min
Orbital period
440.03 mins
BSTAR
0.00070237
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Other satellites on launch #60 in the year 2014 (2014-10-07 UTC)

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