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 (10 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: 2 days ago

TLE from 2 days ago

0 H-2A R/B
1 41837U 16064B   26171.43155870  .00042502 -16049-6  15914-2 0  9992
2 41837  22.3944 219.9153 6349955  33.3912 354.0344  3.59051894 98106

Epoch: 2026-06-20T10:21Z

TLE epoch observation values (Epoch: 2026-06-20T10:21:26.671Z)

Latitude

-0.00009°

Longitude

155.92166°

Altitude

637.333 km

Speed

9.566 km/s

True Right ascension

14h 39m 42s

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

21:38:07

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

23,082.844 km

Perigee altitude

198.878 km

Semi-major axis

18,018.998 km

Eccentricity

0.635

Inclination

22.3944°

RAAN

219.9153°

Arg. of periapsis

33.3912°

True anomaly

326.90052°

Mean anomaly

354.0344°

Eccentric anomaly

344.01542°

Mean motion

0.89732 °/min

Orbital period

401.19 mins

BSTAR

0.0015914

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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.
284 mins	2026-06-22 16:32:04.830Z	252.346° W	2026-06-22 17:29:04.830Z	216.87° SW	25.229°	2026-06-22 21:16:04.830Z	193.678° SSW

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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: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-06-20T10:21:26.671Z)

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: 2 days ago