H-2A DEB, 43068

Orbit data source: Space-Track

H-2A DEB, 43068 is space debris in SSO originally from a launch on Sat, 23 Dec 2017 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.

Not visible in the next 10 days

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Iframe URL

https://www.satcat.com/sats-embedded/43068?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

43068, 2017-082D

Orbit

SSO

Country

JP / JPN

Related business

JAXA (Japan Aerospace Exploration Agency) (JP)

Manufacturer

MELCO

Mission

Spacecraft

Bus & Motor

Unknown

Mass

~50 kg wet, ~50 kg dry

Launch date (UTC)

2017-12-23 (8 years ago)

Launch vehicle

Unknown

Launch site

Tanegashima Space Center (TNSTA)

Object type

Payload

Rocket body

Debris

Shape & HBR

Trunc Cone, 0.5 m

Radar Cross Section

0.533 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago

0 H-2A DEB
1 43068U 17082D   26002.19463802  .01363472  10827-2  22492-2 0  9999
2 43068  97.9909 172.8829 0011321 119.4300 240.8109 16.03256746437928

Epoch: 2026-01-02T04:40Z

TLE epoch observation values (Epoch: 2026-01-02T04:40:16.724Z)

Latitude

-0.0001°

Longitude

0.97488°

Altitude

272.266 km

Speed

7.742 km/s

True Right ascension

11h 31m 31s

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

19:42:53

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

269.807 km

Perigee altitude

254.772 km

Semi-major axis

6,640.426 km

Eccentricity

0.00113

Inclination

97.9909°

RAAN

172.8829°

Arg. of periapsis

119.43°

True anomaly

240.69772°

Mean anomaly

240.8109°

Eccentric anomaly

240.7543°

Mean motion

4.01097 °/min

Orbital period

89.75 mins

BSTAR

0.0022492

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Other satellites on launch #82 in the year 2017 (2017-12-23 UTC)

H-2A R/B, 43067 (Decayed)

GCOM-C, 43065

SLATS, 43066 (Decayed)

H-2A DEB, 43069

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H-2A DEB Visibility

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H-2A DEB is likely not visible in the next few days.

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 DEB, 43068 on other resources

View H-2A DEB, 43068 on Heavens-Above

View H-2A DEB, 43068 on Keep Track

View H-2A DEB, 43068 on Celestrak

View H-2A DEB, 43068 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 DEB, 43068

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-01-02T04:40:16.724Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #82 in the year 2017 (2017-12-23 UTC)

H-2A DEB Visibility

Co-orbital & Co-planar RSOs

Check out H-2A DEB, 43068 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago