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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https://www.satcat.com/sats-embedded/62877?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

62877, 2025-023B

Orbit

HEO

Last TLE update

3 days ago

Origin

Mitsubishi Heavy Industries (MHI) (JP / JPN)

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 (5 months ago)

Launch vehicle

Unknown

Launch site

Tanegashima Space Center (TNSTA)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 11 m

Radar Cross Section

55.543 m²

Expand to show TLE details & history

TLE from 3 days ago

0 H-3 R/B
1 62877U 25023B   25181.21674782  .00001054  00000-0  75351-3 0  9990
2 62877  21.0278 244.6766 7222980 280.7260  12.0302  2.33156660  3432

Epoch: 2025-06-30T05:12Z

TLE epoch observation values (Epoch: 2025-06-30T05:12:07.011Z)

Latitude

0.00066°

Longitude

-111.7275°

Altitude

3,796.849 km

Speed

7.858 km/s

True Right ascension

16h 19m 19s

True Declination

0° 00' 02"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

16.50623°

Longitude

16.69979°

Altitude

26,875.774 km

Speed

2.717 km/s

Apparent Right ascension

01h 03m 09s

Apparent Declination

8° 21' 09"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

14:10:00

Azimuth

21.574° NNE

Elevation

-39.316°

Doppler factor

Orbital elements

Apogee altitude

35,005.25 km

Perigee altitude

294.488 km

Semi-major axis

24,028.006 km

Eccentricity

0.7223

Inclination

21.0278°

RAAN

244.6766°

Arg. of periapsis

280.726°

True anomaly

Unknown

Mean anomaly

12.0302°

Eccentric anomaly

Unknown

Mean motion

0.58273 °/min

Orbital period

617.78 mins

BSTAR

0.00075351

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

QZS-6, 62876

H-3 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.
566 mins	2025-07-03 05:14:59.191Z	196.013° SSW	2025-07-03 11:35:59.191Z	153.646° SSE	41.619°	2025-07-03 14:40:59.191Z	137.99° SSE

Authenticating...

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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

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