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 (1 year 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: 15 hours ago

TLE from 15 hours ago

0 H-3 R/B
1 62877U 25023B   26084.23871018  .00006048  00000-0  11162-2 0  9993
2 62877  20.7810 136.4056 7234540 113.7310 333.8649  2.34860312  9729

Epoch: 2026-03-25T05:43Z

TLE epoch observation values (Epoch: 2026-03-25T05:43:44.559Z)

Latitude

-0.00001°

Longitude

-132.13266°

Altitude

9,665.31 km

Speed

5.746 km/s

True Right ascension

09h 06m 01s

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

01:28:30

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

34,832.679 km

Perigee altitude

234.564 km

Semi-major axis

23,911.759 km

Eccentricity

0.72345

Inclination

20.781°

RAAN

136.4056°

Arg. of periapsis

113.731°

True anomaly

246.23955°

Mean anomaly

333.8649°

Eccentric anomaly

296.8987°

Mean motion

0.58698 °/min

Orbital period

613.31 mins

BSTAR

0.0011162

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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.
370 mins	2026-03-25 20:15:46.490Z	144.023° SSE	2026-03-26 01:28:46.490Z	162.088° S	24.375°	2026-03-26 02:25:46.490Z	122.43° SE

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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: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-03-25T05:43:44.559Z)

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: 15 hours ago