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

Last TLE update

1 day ago

Origin

Mitsubishi Heavy Industries (MHI) (JP / JPN)

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 (9 months ago)

Launch vehicle

Unknown

Launch site

Tanegashima Space Center (TNSTA)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 9.2 m

Radar Cross Section

35.186 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 H-2A R/B
1 61440U 24176B   25169.91704597  .00021449  00000-0  49996-3 0  9990
2 61440  97.2432 300.1997 0014020 176.3662 183.7690 15.42165720 40721

Epoch: 2025-06-18T22:00Z

TLE epoch observation values (Epoch: 2025-06-18T22:00:32.771Z)

Latitude

-0.00004°

Longitude

62.67095°

Altitude

452.384 km

Speed

7.636 km/s

True Right ascension

20h 00m 47s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-82.53202°

Longitude

169.18956°

Altitude

468.919 km

Speed

7.63 km/s

Apparent Right ascension

00h 54m 50s

Apparent Declination

-62° 34' 44"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:32:03

Azimuth

186.741° SSW

Elevation

-67.079°

Doppler factor

Orbital elements

Apogee altitude

446.203 km

Perigee altitude

427.094 km

Semi-major axis

6,814.785 km

Eccentricity

0.0014

Inclination

97.2432°

RAAN

300.1997°

Arg. of periapsis

176.3662°

True anomaly

Unknown

Mean anomaly

183.769°

Eccentric anomaly

Unknown

Mean motion

3.85802 °/min

Orbital period

93.31 mins

BSTAR

0.00049996

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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)

H-2A R/B Visibility forecast

Observer location: undefined°, undefined°

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	2025-06-20 08:24:25.198Z	141.632° SSE	2025-06-20 08:26:25.198Z	95.609° ESE	33.226°	2025-06-20 08:29:25.198Z	5.546° NNE
4 mins	2025-06-20 21:18:25.198Z	36.59° NE	2025-06-20 21:20:25.198Z	130.398° SE	35.1°	2025-06-20 21:22:25.198Z	172.476° S

Authenticating...

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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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