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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Iframe URL

https://www.satcat.com/sats-embedded/40268?theme=dark&initialShowStats=false

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Identifier

40268, 2014-060B

Orbit

HEO

Country

JP / JPN

Related business

Mitsubishi Heavy Industries (MHI) (JP)

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 (11 years ago)

Launch vehicle

Unknown

Launch site

Tanegashima Space Center (TNSTA)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 4.6 m

Radar Cross Section

35.186 m², Large (>1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 H-2A R/B
1 40268U 14060B   25341.76274039  .00012845  00000-0  14651-2 0  9993
2 40268  22.6596  36.9645 6648270 280.8865  15.7815  3.13521222107775

Epoch: 2025-12-07T18:18Z

TLE epoch observation values (Epoch: 2025-12-07T18:18:20.769Z)

Latitude

0.00061°

Longitude

45.61201°

Altitude

3,418.275 km

Speed

7.82 km/s

True Right ascension

02h 27m 52s

True Declination

0° 00' 02"

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

17:26:54

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

26,457.97 km

Perigee altitude

232.626 km

Semi-major axis

19,723.435 km

Eccentricity

0.66483

Inclination

22.6596°

RAAN

36.9645°

Arg. of periapsis

280.8865°

True anomaly

78.9161°

Mean anomaly

15.7815°

Eccentric anomaly

40.5407°

Mean motion

0.78355 °/min

Orbital period

459.44 mins

BSTAR

0.0014651

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Other satellites on launch #60 in the year 2014 (2014-10-07 UTC)

HIMAWARI 8, 40267

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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.
397 mins	2025-12-09 08:48:11.211Z	245.695° WSW	2025-12-09 11:17:11.211Z	218.66° SW	41.955°	2025-12-09 15:25:11.211Z	154.633° SSE

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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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Check out H-2A R/B, 40268 on other resources

View H-2A R/B, 40268 on Heavens-Above

View H-2A R/B, 40268 on Keep Track

View H-2A R/B, 40268 on Celestrak

View H-2A R/B, 40268 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

H-2A R/B, 40268

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2025-12-07T18:18:20.769Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #60 in the year 2014 (2014-10-07 UTC)

H-2A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out H-2A R/B, 40268 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago