ASIASAT 2 PKM, 23725

Orbit data source: Space-Track

ASIASAT 2 PKM, 23725 is space debris in HEO originally from a launch on Tue, 28 Nov 1995 UTC launched from the Xichang Space Center, China (XSC). 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 src="https://www.satcat.com/sats-embedded/23725?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/23725?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

23725, 1995-064C

Orbit

HEO

Last TLE update

1 day ago

Origin

China Aerospace Science and Technology Corporation (CASC) (CN / PRC)

Manufacturer

China ARMT

Mission

Spacecraft

Bus & Motor

FG-46, Unknown motor

Mass

5,985 kg wet, 541 kg dry

Launch date (UTC)

1995-11-28 (30 years ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + Cone, 3.07 m

Radar Cross Section

5.234 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 ASIASAT 2 PKM
1 23725U 95064C   25162.54760270  .00007075  00000-0  10418-2 0  9995
2 23725  25.7592 254.4262 5526501 163.4991 226.2731  4.78136006429804

Epoch: 2025-06-11T13:08Z

TLE epoch observation values (Epoch: 2025-06-11T13:08:32.873Z)

Latitude

0.0001°

Longitude

157.16296°

Altitude

15,613.726 km

Speed

3.078 km/s

True Right ascension

16h 57m 42s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-23.37491°

Longitude

39.13981°

Altitude

3,053.847 km

Speed

7.6 km/s

Apparent Right ascension

11h 00m 05s

Apparent Declination

-37° 22' 20"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

02:51:32

Azimuth

106.105° ESE

Elevation

-45.538°

Doppler factor

Orbital elements

Apogee altitude

16,736.211 km

Perigee altitude

281.574 km

Semi-major axis

14,887.03 km

Eccentricity

0.55265

Inclination

25.7592°

RAAN

254.4262°

Arg. of periapsis

163.4991°

True anomaly

Unknown

Mean anomaly

226.2731°

Eccentric anomaly

Unknown

Mean motion

1.1949 °/min

Orbital period

301.28 mins

BSTAR

0.0010418

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Other satellites on launch #64 in the year 1995 (1995-11-28 UTC)

AMOS 5I (ASIASAT 2), 23723

CZ-2E R/B, 23724 (Decayed)

ASIASAT 2 DEB, 28062 (Decayed)

ASIASAT 2 DEB, 28063 (Decayed)

ASIASAT 2 PKM 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.
194 mins	2025-06-13 03:21:00.857Z	182.69° SSW	2025-06-13 05:44:00.857Z	139.935° SSE	29.915°	2025-06-13 06:35:00.857Z	94.524° ESE
94 mins	2025-06-13 10:23:00.857Z	247.969° W	2025-06-13 11:47:00.857Z	190.793° SSW	38.467°	2025-06-13 11:57:00.857Z	119.172° SE

Authenticating...

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Check out ASIASAT 2 PKM, 23725 on other resources

View ASIASAT 2 PKM, 23725 on Heavens-Above

View ASIASAT 2 PKM, 23725 on Keep Track

View ASIASAT 2 PKM, 23725 on Celestrak

View ASIASAT 2 PKM, 23725 on Gunter's Space Page

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