H-2A R/B, 41837

Orbit data source: Space-Track

H-2A R/B, 41837 is space debris in HEO originally from a launch on Wed, 02 Nov 2016 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/41837?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41837, 2016-064B

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)

2016-11-02 (9 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: 16 hours ago

TLE from 16 hours ago

0 H-2A R/B
1 41837U 16064B   25330.73014420  .00012743  00000-0  12158-2 0  9990
2 41837  22.6157 357.4207 6392292 150.4272 270.0113  3.50075150 90829

Epoch: 2025-11-26T17:31Z

TLE epoch observation values (Epoch: 2025-11-26T17:31:24.458Z)

Latitude

0.00001°

Longitude

28.6716°

Altitude

18,012.942 km

Speed

3.306 km/s

True Right ascension

23h 49m 40s

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

07:15:15

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

23,661.76 km

Perigee altitude

233.213 km

Semi-major axis

18,325.623 km

Eccentricity

0.63923

Inclination

22.6157°

RAAN

357.4207°

Arg. of periapsis

150.4272°

True anomaly

209.56353°

Mean anomaly

270.0113°

Eccentric anomaly

238.71248°

Mean motion

0.87489 °/min

Orbital period

411.48 mins

BSTAR

0.0012158

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Other satellites on launch #64 in the year 2016 (2016-11-02 UTC)

HIMAWARI 9, 41836

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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.
296 mins	2025-11-28 00:17:27.760Z	208.744° SW	2025-11-28 04:52:27.760Z	176.992° S	36.033°	2025-11-28 05:13:27.760Z	109.517° ESE

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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, 41837 on other resources

View H-2A R/B, 41837 on Heavens-Above

View H-2A R/B, 41837 on Keep Track

View H-2A R/B, 41837 on Celestrak

View H-2A R/B, 41837 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, 41837

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2025-11-26T17:31:24.458Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #64 in the year 2016 (2016-11-02 UTC)

H-2A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out H-2A R/B, 41837 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago