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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Iframe URL

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)

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Last TLE update: 10 hours ago

TLE from 10 hours ago

0 H-2A R/B
1 61440U 24176B   26020.32641574  .00079546  00000-0  90092-3 0  9991
2 61440  97.2607 157.0436 0007823 109.1579 251.0527 15.62118124 74099

Epoch: 2026-01-20T07:50Z

TLE epoch observation values (Epoch: 2026-01-20T07:50:02.319Z)

Latitude

-0.00002°

Longitude

-80.17595°

Altitude

386.412 km

Speed

7.677 km/s

True Right ascension

10h 28m 10s

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

18:30:19

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

383.729 km

Perigee altitude

373.158 km

Semi-major axis

6,756.58 km

Eccentricity

0.00078

Inclination

97.2607°

RAAN

157.0436°

Arg. of periapsis

109.1579°

True anomaly

250.96794°

Mean anomaly

251.0527°

Eccentric anomaly

251.01032°

Mean motion

3.90798 °/min

Orbital period

92.12 mins

BSTAR

0.00090092

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

IGS R-8, 61439

H-2A DEB, 61442 (Decayed)

H-2A DEB, 61441 (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	2026-01-20 22:13:22.543Z	351.666° N	2026-01-20 22:15:22.543Z	302.432° NW	30.452°	2026-01-20 22:18:22.543Z	216.512° SW

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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

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H-2A R/B, 61440

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-01-20T07:50:02.319Z)

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: 10 hours ago