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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https://www.satcat.com/sats-embedded/41837?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41837, 2016-064B

Orbit

HEO

Last TLE update

12 hours ago

Origin

Mitsubishi Heavy Industries (MHI) (JP / JPN)

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, 9.2 m

Radar Cross Section

35.186 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 12 hours ago

0 H-2A R/B
1 41837U 16064B   25168.14646323  .00047880 -26894-6  16498-2 0  9994
2 41837  22.4661 103.3986 6462902 323.3959   6.3695  3.42924509 85177

Epoch: 2025-06-17T03:30Z

TLE epoch observation values (Epoch: 2025-06-17T03:30:54.423Z)

Latitude

0.00006°

Longitude

144.98514°

Altitude

736.436 km

Speed

9.518 km/s

True Right ascension

06h 53m 26s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

5.66483°

Longitude

-49.18086°

Altitude

20,882.129 km

Speed

2.79 km/s

Apparent Right ascension

17h 24m 15s

Apparent Declination

-2° 39' 01"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

01:58:07

Azimuth

294.912° NW

Elevation

-30.415°

Doppler factor

Orbital elements

Apogee altitude

24,209.1 km

Perigee altitude

193.612 km

Semi-major axis

18,579.493 km

Eccentricity

0.64629

Inclination

22.4661°

RAAN

103.3986°

Arg. of periapsis

323.3959°

True anomaly

Unknown

Mean anomaly

6.3695°

Eccentric anomaly

Unknown

Mean motion

0.85702 °/min

Orbital period

420.06 mins

BSTAR

0.0016498

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

HIMAWARI 9, 41836

H-2A R/B Visibility forecast

Observer location: undefined°, undefined°

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.
342 mins	2025-06-18 00:42:04.897Z	235.06° WSW	2025-06-18 01:10:04.897Z	160.158° S	40.824°	2025-06-18 06:24:04.897Z	131.561° SE

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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

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