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: 3 days ago

TLE from 3 days ago

0 H-2A R/B
1 41837U 16064B   25269.51635411  .00015908  00000-0  14394-2 0  9996
2 41837  22.6061  37.3800 6405554  79.9190 342.1521  3.48367368 88683

Epoch: 2025-09-26T12:23Z

TLE epoch observation values (Epoch: 2025-09-26T12:23:32.995Z)

Latitude

0.00006°

Longitude

-154.1006°

Altitude

3,380.631 km

Speed

7.746 km/s

True Right ascension

02h 29m 23s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

14:42:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

23,784.225 km

Perigee altitude

230.416 km

Semi-major axis

18,385.457 km

Eccentricity

0.64056

Inclination

22.6061°

RAAN

37.38°

Arg. of periapsis

79.919°

True anomaly

280.16849°

Mean anomaly

342.1521°

Eccentric anomaly

317.2299°

Mean motion

0.87063 °/min

Orbital period

413.5 mins

BSTAR

0.0014394

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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.
326 mins	2025-09-30 00:10:02.887Z	217.589° SW	2025-09-30 01:22:02.887Z	192.518° SSW	15.523°	2025-09-30 05:36:02.887Z	154.778° SSE
46 mins	2025-09-30 20:21:02.887Z	208.754° SW	2025-09-30 20:31:02.887Z	177.413° S	17.394°	2025-09-30 21:07:02.887Z	148.487° SSE

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: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2025-09-26T12:23:32.995Z)

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: 3 days ago