H-2A R/B, 61440

Orbit data source: Space-Track

H-2A R/B, 61440 is space debris in SSO originally from a launch on Thu, 26 Sep 2024 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/61440?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61440, 2024-176B

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)

2024-09-26 (1 year 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)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago

0 H-2A R/B
1 61440U 24176B   25340.85714308  .00075837  00000-0  10538-2 0  9994
2 61440  97.2607 111.6114 0009162 273.5849  86.4358 15.56703737 67167

Epoch: 2025-12-06T20:34Z

TLE epoch observation values (Epoch: 2025-12-06T20:34:17.162Z)

Latitude

-0.00004°

Longitude

87.16103°

Altitude

399.968 km

Speed

7.671 km/s

True Right ascension

07h 26m 26s

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

13:47:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

400.32 km

Perigee altitude

387.911 km

Semi-major axis

6,772.252 km

Eccentricity

0.00092

Inclination

97.2607°

RAAN

111.6114°

Arg. of periapsis

273.5849°

True anomaly

86.54059°

Mean anomaly

86.4358°

Eccentric anomaly

86.4882°

Mean motion

3.89443 °/min

Orbital period

92.44 mins

BSTAR

0.0010538

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Other satellites on launch #176 in the year 2024 (2024-09-26 UTC)

IGS R-8, 61439

H-2A DEB, 61441 (Decayed)

H-2A DEB, 61442 (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.
5 mins	2025-12-07 21:48:22.037Z	9.136° NNE	2025-12-07 21:51:22.037Z	226.821° WSW	43.619°	2025-12-07 21:53:22.037Z	197.001° 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, 61440 on other resources

View H-2A R/B, 61440 on Heavens-Above

View H-2A R/B, 61440 on Keep Track

View H-2A R/B, 61440 on Celestrak

View H-2A R/B, 61440 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, 61440

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2025-12-06T20:34:17.162Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #176 in the year 2024 (2024-09-26 UTC)

H-2A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out H-2A R/B, 61440 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 19 hours ago