H-2 R/B(2), 23523

Orbit data source: Space-Track

H-2 R/B(2), 23523 is space debris in HEO originally from a launch on Sat, 18 Mar 1995 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/23523?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

23523, 1995-011C

Orbit

HEO

Last TLE update

1 day ago

Origin

JAXA (Japan Aerospace Exploration Agency) (JP / JPN)

Manufacturer

MHI Tobishima

Mission

Spacecraft

Bus & Motor

LE-5A, Unknown motor

Mass

~3,030 kg wet, 2,700 kg dry

Launch date (UTC)

1995-03-18 (30 years ago)

Launch vehicle

Unknown

Launch site

Tanegashima Space Center (TNSTA)

Object type

Payload

Rocket body

Debris

Shape & HBR

Sphere + Cyl, 11.69 m

Radar Cross Section

43.008 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 H-2 R/B(2)
1 23523U 95011C   25158.05130186  .00011439  00000-0  13798-2 0  9994
2 23523  25.1388 176.8013 6495002 283.0617  16.1705  3.34636900321553

Epoch: 2025-06-07T01:13Z

TLE epoch observation values (Epoch: 2025-06-07T01:13:52.48Z)

Latitude

0.00002°

Longitude

-97.3095°

Altitude

3,147.644 km

Speed

7.91 km/s

True Right ascension

11h 47m 25s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

24.14696°

Longitude

-25.42039°

Altitude

18,546.397 km

Speed

3.298 km/s

Apparent Right ascension

16h 20m 54s

Apparent Declination

18° 44' 22"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

17:27:06

Azimuth

218.747° SW

Elevation

64.474°

Doppler factor

Orbital elements

Apogee altitude

24,772.071 km

Perigee altitude

240.923 km

Semi-major axis

18,884.634 km

Eccentricity

0.6495

Inclination

25.1388°

RAAN

176.8013°

Arg. of periapsis

283.0617°

True anomaly

Unknown

Mean anomaly

16.1705°

Eccentric anomaly

Unknown

Mean motion

0.83634 °/min

Orbital period

430.45 mins

BSTAR

0.0013798

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Other satellites on launch #11 in the year 1995 (1995-03-18 UTC)

SFU, 23521 (Decayed)

HIMAWARI 5 (GMS 5), 23522

HIMAWARI 5 AKM, 23524

H-2 R/B(1), 23525 (Decayed)

SFU DEB, 23569 (Decayed)

SFU DEB, 23570 (Decayed)

SFU DEB, 23593 (Decayed)

SFU DEB, 23771 (Decayed)

SFU DEB, 23772 (Decayed)

H-2 R/B(2) 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.
295 mins	2025-06-08 07:19:50.637Z	218.701° SW	2025-06-08 08:37:50.637Z	206.719° SW	43.107°	2025-06-08 12:14:50.637Z	145.759° SSE
230 mins	2025-06-09 03:29:50.637Z	211.475° SW	2025-06-09 04:21:50.637Z	134.348° SE	40.071°	2025-06-09 07:19:50.637Z	115.869° SE

Authenticating...

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Check out H-2 R/B(2), 23523 on other resources

View H-2 R/B(2), 23523 on Heavens-Above

View H-2 R/B(2), 23523 on Keep Track

View H-2 R/B(2), 23523 on Celestrak

View H-2 R/B(2), 23523 on Gunter's Space Page

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