H-2A R/B, 43682

Orbit data source: Space-Track

H-2A R/B, 43682 is space debris in SSO originally from a launch on Mon, 29 Oct 2018 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/43682?theme=dark&initialShowStats=false

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Identifier

43682, 2018-084L

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)

2018-10-29 (8 years ago)

Launch vehicle

Unknown

Launch site

Tanegashima Space Center (TNSTA)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 5.0 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 43682U 18084L   26277.62541528  .00022059  00000-0  40373-3 0  9999
2 43682  98.8395 180.7013 0021258  18.1791 342.0211 15.49135693438040

Epoch: 2026-10-04T15:00Z

TLE epoch observation values (Epoch: 2026-10-04T15:00:35.880Z)

Latitude

0.00002°

Longitude

-57.76418°

Altitude

408.593 km

Speed

7.673 km/s

True Right ascension

12h 02m 48s

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

13:49:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

430.692 km

Perigee altitude

401.805 km

Semi-major axis

6,794.385 km

Eccentricity

0.00213

Inclination

98.8395°

RAAN

180.7013°

Arg. of periapsis

18.1791°

True anomaly

341.94572°

Mean anomaly

342.0211°

Eccentric anomaly

341.98343°

Mean motion

3.87541 °/min

Orbital period

92.89 mins

BSTAR

0.00040373

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Other satellites on launch #84 in the year 2018 (2018-10-29 UTC)

H-2A DEB, 47191 (Decayed)

H-2A DEB, 53331 (Decayed)

H-2A DEB, 53329 (Decayed)

H-2A DEB, 53117 (Decayed)

H-2A DEB, 44052 (Decayed)

H-2A DEB, 46208 (Decayed)

H-2A DEB, 53335 (Decayed)

H-2A DEB, 46187 (Decayed)

H-2A DEB, 53115 (Decayed)

H-2A DEB *, 48551

H-2A DEB, 46221 (Decayed)

H-2A DEB, 46228 (Decayed)

H-2A DEB, 46414 (Decayed)

KHALIFASAT, 43676

H-2A DEB, 53338 (Decayed)

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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.
4 mins	2026-10-05 07:04:57.982Z	336.068° NNW	2026-10-05 07:05:57.982Z	304.641° NW	34.169°	2026-10-05 07:08:57.982Z	223.693° SW
4 mins	2026-10-05 17:30:57.982Z	145.933° SSE	2026-10-05 17:31:57.982Z	110.29° ESE	58.542°	2026-10-05 17:34:57.982Z	353.788° 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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Check out H-2A R/B, 43682 on other resources

View H-2A R/B, 43682 on Heavens-Above

View H-2A R/B, 43682 on Keep Track

View H-2A R/B, 43682 on Celestrak

View H-2A R/B, 43682 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, 43682

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: 2026-10-04T15:00:35.880Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #84 in the year 2018 (2018-10-29 UTC)

H-2A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out H-2A R/B, 43682 on other resources

Documentation

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