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.

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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)

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Last TLE update: 7 hours ago

TLE from 7 hours ago

0 H-2A DEB
1 43068U 17082D   25306.43191189  .00118964  00000-0  12677-2 0  9995
2 43068  98.0045 102.7976 0053865 352.1362   7.9043 15.61746389428355

Epoch: 2025-11-02T10:21Z

TLE epoch observation values (Epoch: 2025-11-02T10:21:57.187Z)

Latitude

-0.00004°

Longitude

-94.6384°

Altitude

349.666 km

Speed

7.72 km/s

True Right ascension

06h 51m 11s

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

12:45:03

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

415.95 km

Perigee altitude

343.149 km

Semi-major axis

6,757.687 km

Eccentricity

0.00539

Inclination

98.0045°

RAAN

102.7976°

Arg. of periapsis

352.1362°

True anomaly

7.98975°

Mean anomaly

7.9043°

Eccentric anomaly

7.94697°

Mean motion

3.90702 °/min

Orbital period

92.14 mins

BSTAR

0.0012677

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

GCOM-C, 43065

SLATS, 43066 (Decayed)

H-2A DEB, 43069

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

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H-2A DEB 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.
5 mins	2025-11-02 23:13:39.934Z	28.753° NE	2025-11-02 23:15:39.934Z	84.12° E	36.865°	2025-11-02 23:18:39.934Z	176.454° S

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: 7 hours ago

TLE from 7 hours ago

TLE epoch observation values (Epoch: 2025-11-02T10:21:57.187Z)

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 forecast

Co-orbital & Co-planar RSOs

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

Documentation

Expand to show TLE details & history
Last TLE update: 7 hours ago