H-3 R/B, 62877

Orbit data source: Space-Track

H-3 R/B, 62877 is space debris in HEO originally from a launch on Sun, 02 Feb 2025 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/62877?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

62877, 2025-023B

Orbit

HEO

Country

JP / JPN

Related business

Mitsubishi Heavy Industries (MHI) (JP)

Manufacturer

MHI Tobishima

Mission

Spacecraft

Bus & Motor

H-2A STAGE 2, Unknown motor

Mass

2,500 kg wet, 2,500 kg dry

Launch date (UTC)

2025-02-02 (11 months ago)

Launch vehicle

Unknown

Launch site

Tanegashima Space Center (TNSTA)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 5.6 m

Radar Cross Section

55.543 m², Large (>1 m²)

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Last TLE update: 18 hours ago

TLE from 18 hours ago

0 H-3 R/B
1 62877U 25023B   25357.99979141  .00002456  00000-0  11674-2 0  9991
2 62877  20.8432 174.1370 7220802  47.0657 354.2948  2.34184517  7584

Epoch: 2025-12-23T23:59Z

TLE epoch observation values (Epoch: 2025-12-23T23:59:41.977Z)

Latitude

0.00013°

Longitude

81.31527°

Altitude

1,316.662 km

Speed

9.325 km/s

True Right ascension

11h 36m 03s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

17:01:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

34,878.922 km

Perigee altitude

280.179 km

Semi-major axis

23,957.687 km

Eccentricity

0.72208

Inclination

20.8432°

RAAN

174.137°

Arg. of periapsis

47.0657°

True anomaly

313.57919°

Mean anomaly

354.2948°

Eccentric anomaly

340.45146°

Mean motion

0.5853 °/min

Orbital period

615.07 mins

BSTAR

0.0011674

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Other satellites on launch #23 in the year 2025 (2025-02-02 UTC)

QZS-6, 62876

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H-3 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.
534 mins	2025-12-24 20:51:31.875Z	233.05° WSW	2025-12-24 21:02:31.875Z	170.707° S	30.801°	2025-12-25 05:45:31.875Z	161.774° S

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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-3 R/B, 62877 on other resources

View H-3 R/B, 62877 on Heavens-Above

View H-3 R/B, 62877 on Keep Track

View H-3 R/B, 62877 on Celestrak

View H-3 R/B, 62877 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-3 R/B, 62877

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 18 hours ago

TLE from 18 hours ago

TLE epoch observation values (Epoch: 2025-12-23T23:59:41.977Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #23 in the year 2025 (2025-02-02 UTC)

H-3 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out H-3 R/B, 62877 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 18 hours ago