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ARIANE 2 DEB, 28567

Orbit data source: Space-Track

ARIANE 2 DEB, 28567 is space debris in HEO originally from a launch on Fri, 27 Jan 1989 UTC launched from the French Guiana (FRGUI). 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/28567?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

28567, 1989-006AJ

Orbit

HEO

Country

FR

Related business

ArianeGroup (FR)

Manufacturer

EADS/LV

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1989-01-27 (37 years ago)

Launch vehicle

Unknown

Launch site

French Guiana (FRGUI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 1.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 ARIANE 2 DEB
1 28567U 89006AJ  25362.63090302  .00000004  00000-0 -15055-3 0  9996
2 28567   8.1172  32.5982 7088083 169.6292 221.5887  2.38005324116421

Epoch: 2025-12-28T15:08Z

TLE epoch observation values (Epoch: 2025-12-28T15:08:30.020Z)

Latitude

0.00001°

Longitude

68.09862°

Altitude

32,570.311 km

Speed

1.91 km/s

True Right ascension

02h 10m 15s

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

02:20:36

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

34,122.808 km

Perigee altitude

523.479 km

Semi-major axis

23,701.28 km

Eccentricity

0.70881

Inclination

8.1172°

RAAN

32.5982°

Arg. of periapsis

169.6292°

True anomaly

190.30777°

Mean anomaly

221.5887°

Eccentric anomaly

204.65037°

Mean motion

0.59482 °/min

Orbital period

605.23 mins

BSTAR

-0.00015055

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Other satellites on launch #6 in the year 1989 (1989-01-27 UTC)

ARIANE 2 DEB, 42482

ARIANE 2 DEB, 33571

ARIANE 2 DEB, 33560

ARIANE 2 DEB, 33582

ARIANE 2 DEB, 26727

ARIANE 2 DEB, 42487

ARIANE 2 DEB, 27602

ARIANE 2 DEB, 42485

ARIANE 2 DEB, 27042

ARIANE 2 DEB, 33552 (Decayed)

INTELSAT 515, 19772

ARIANE 2 DEB, 27045

ARIANE 2 DEB, 40783

ARIANE 2 DEB, 33568

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

ARIANE 2 DEB 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.
104 mins	2025-12-29 02:49:47.879Z	155.537° SSE	2025-12-29 02:52:47.879Z	155.534° SSE	33.456°	2025-12-29 04:33:47.879Z	117.912° 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 ARIANE 2 DEB, 28567 on other resources

View ARIANE 2 DEB, 28567 on Heavens-Above

View ARIANE 2 DEB, 28567 on Keep Track

View ARIANE 2 DEB, 28567 on Celestrak

View ARIANE 2 DEB, 28567 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

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