ARIANE 2 DEB, 26726

Orbit data source: Space-Track

ARIANE 2 DEB, 26726 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/26726?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26726, 1989-006D

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, 0.5 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago

0 ARIANE 2 DEB
1 26726U 89006D   25349.80734640  .00000019  00000-0  81715-3 0  9996
2 26726   7.6124 167.7841 7179654 258.6517  27.1152  2.27630338207047

Epoch: 2025-12-15T19:22Z

TLE epoch observation values (Epoch: 2025-12-15T19:22:34.728Z)

Latitude

1.70261°

Longitude

165.26134°

Altitude

10,359.916 km

Speed

5.594 km/s

True Right ascension

12h 02m 25s

True Declination

1° 41' 54"

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

03:12:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,567.722 km

Perigee altitude

508.022 km

Semi-major axis

24,416.009 km

Eccentricity

0.71797

Inclination

7.6124°

RAAN

167.7841°

Arg. of periapsis

258.6517°

True anomaly

114.2105°

Mean anomaly

27.1152°

Eccentric anomaly

64.12878°

Mean motion

0.56889 °/min

Orbital period

632.81 mins

BSTAR

0.00081715

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

ARIANE 2 DEB, 26727

ARIANE 2 DEB, 33560

ARIANE 2 DEB, 33582

ARIANE 2 DEB, 40786

ARIANE 2 DEB, 33565

ARIANE 2 DEB, 26728

ARIANE 2 DEB, 27040

ARIANE 2 DEB, 33561

ARIANE 2 DEB, 33568

ARIANE 2 DEB, 33574

ARIANE 2 R/B, 19773

ARIANE 2 DEB, 33558

ARIANE 2 DEB, 26717

ARIANE 2 DEB, 33557

ARIANE 2 DEB, 27032

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

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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.
560 mins	2025-12-16 16:26:53.995Z	240.469° WSW	2025-12-16 18:26:53.995Z	230.536° WSW	30.911°	2025-12-17 01:46:53.995Z	221.255° SW

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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, 26726 on other resources

View ARIANE 2 DEB, 26726 on Heavens-Above

View ARIANE 2 DEB, 26726 on Keep Track

View ARIANE 2 DEB, 26726 on Celestrak

View ARIANE 2 DEB, 26726 on Gunter's Space Page

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

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