H-2A R/B, 38341

Orbit data source: Space-Track

H-2A R/B, 38341 is space debris in SSO originally from a launch on Thu, 17 May 2012 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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https://www.satcat.com/sats-embedded/38341?theme=dark&initialShowStats=false

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Identifier

38341, 2012-025E

Orbit

SSO

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)

2012-05-17 (14 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)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago

0 H-2A R/B
1 38341U 12025E   25354.80810725  .00001641  00000-0  15555-3 0  9995
2 38341  98.4608 310.6606 0044300 209.4230 150.4494 14.94491632736432

Epoch: 2025-12-20T19:23Z

TLE epoch observation values (Epoch: 2025-12-20T19:23:40.466Z)

Latitude

0.00001°

Longitude

-69.88761°

Altitude

613.844 km

Speed

7.538 km/s

True Right ascension

20h 42m 38s

True Declination

0° 00' 00"

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

23:20:53

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

611.828 km

Perigee altitude

550.17 km

Semi-major axis

6,959.136 km

Eccentricity

0.00443

Inclination

98.4608°

RAAN

310.6606°

Arg. of periapsis

209.423°

True anomaly

150.69856°

Mean anomaly

150.4494°

Eccentric anomaly

150.5741°

Mean motion

3.73861 °/min

Orbital period

96.29 mins

BSTAR

0.00015555

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Other satellites on launch #25 in the year 2012 (2012-05-17 UTC)

H-2A DEB, 54717 (Decayed)

H-2A DEB, 54718 (Decayed)

H-2A DEB, 38347

H-2A DEB, 54735 (Decayed)

HORYU 2, 38340

H-2A DEB, 54728 (Decayed)

H-2A DEB, 54712 (Decayed)

GCOM W1, 38337

H-2A DEB, 54729 (Decayed)

H-2A DEB, 54722 (Decayed)

H-2A DEB, 54724 (Decayed)

H-2A DEB, 39007 (Decayed)

H-2A DEB, 54739 (Decayed)

H-2A DEB, 54703 (Decayed)

SDS-4, 38339

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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.
7 mins	2025-12-21 10:25:01.318Z	4.303° NNE	2025-12-21 10:29:01.318Z	264.363° W	39.722°	2025-12-21 10:32:01.318Z	209.551° SW
7 mins	2025-12-21 21:14:01.318Z	166.346° S	2025-12-21 21:17:01.318Z	180.191° SSW	44.835°	2025-12-21 21:21:01.318Z	346.345° N

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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, 38341 on other resources

View H-2A R/B, 38341 on Heavens-Above

View H-2A R/B, 38341 on Keep Track

View H-2A R/B, 38341 on Celestrak

View H-2A R/B, 38341 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, 38341

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 5 hours ago

TLE from 5 hours ago

TLE epoch observation values (Epoch: 2025-12-20T19:23:40.466Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #25 in the year 2012 (2012-05-17 UTC)

H-2A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out H-2A R/B, 38341 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 5 hours ago