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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40268 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated 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)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 5.0 m
Radar Cross Section
35.186 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 H-2A R/B
1 40268U 14060B 26286.95941687 .00011361 00000-0 75726-3 0 9996
2 40268 22.3565 213.5933 6561623 244.9702 35.7011 3.27127654117753Epoch: 2026-10-13T23:01Z
TLE epoch observation values (Epoch: 2026-10-13T23:01:33.617Z)
Latitude
0.00016°
Longitude
-154.29628°
Altitude
8,759.891 km
Speed
5.645 km/s
True Right ascension
14h 14m 26s
True Declination
0° 00' 01"
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
14:08:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
25,375.125 km
Perigee altitude
214.193 km
Semi-major axis
19,172.796 km
Eccentricity
0.65616
Inclination
22.3565°
RAAN
213.5933°
Arg. of periapsis
244.9702°
True anomaly
115.16158°
Mean anomaly
35.7011°
Eccentric anomaly
71.31492°
Mean motion
0.81755 °/min
Orbital period
440.34 mins
BSTAR
0.00075726
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Other satellites on launch #60 in the year 2014 (2014-10-07 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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 378 mins | 2026-10-14 20:53:02.555Z | 216.505° SW | 2026-10-15 01:14:02.555Z | 181.019° SSW | 67.55° | 2026-10-15 03:11:02.555Z | 118.131° SE |
| 47 mins | 2026-10-15 18:48:02.555Z | 185.347° SSW | 2026-10-15 19:35:02.555Z | 140.888° SSE | 40.016° | 2026-10-15 19:35:02.555Z | 140.888° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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