ARIANE 2 R/B, 19122

Orbit data source: Space-Track

ARIANE 2 R/B, 19122 is space debris in HEO originally from a launch on Tue, 17 May 1988 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 src="https://www.satcat.com/sats-embedded/19122?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/19122?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

19122, 1988-040B

Orbit

HEO

Last TLE update

1 day ago

Origin

ArianeGroup (FR)

Manufacturer

Ae/LesM

Mission

Spacecraft

Bus & Motor

ARIANE H10, HM-7B

Mass

1,820 kg wet, 1,820 kg dry

Launch date (UTC)

1988-05-17 (37 years ago)

Launch vehicle

Unknown

Launch site

French Guiana (FRGUI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 5.9 m

Radar Cross Section

26.751 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 ARIANE 2 R/B
1 19122U 88040B   25213.63976905 -.00000082  00000-0 -58251-3 0  9999
2 19122   7.4728  51.7216 7088887 336.6480   2.8348  2.37770338266530

Epoch: 2025-08-01T15:21Z

TLE epoch observation values (Epoch: 2025-08-01T15:21:16.045Z)

Latitude

0°

Longitude

-129.08873°

Altitude

787.53 km

Speed

9.717 km/s

True Right ascension

03h 26m 51s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

3.22451°

Longitude

25.13093°

Altitude

33,982.342 km

Speed

1.715 km/s

Apparent Right ascension

14h 07m 08s

Apparent Declination

-2° 24' 53"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

05:55:08

Azimuth

69.285° E

Elevation

-26.386°

Doppler factor

Orbital elements

Apogee altitude

34,151.427 km

Perigee altitude

526.124 km

Semi-major axis

23,716.913 km

Eccentricity

0.70889

Inclination

7.4728°

RAAN

51.7216°

Arg. of periapsis

336.648°

True anomaly

23.06491°

Mean anomaly

2.8348°

Eccentric anomaly

9.62768°

Mean motion

0.59423 °/min

Orbital period

605.82 mins

BSTAR

-0.00058251

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Other satellites on launch #40 in the year 1988 (1988-05-17 UTC)

NSS 513 (INTELSAT 513), 19121

ARIANE 2 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.
537 mins	2025-08-02 22:10:35.169Z	244.935° WSW	2025-08-02 23:58:35.169Z	217.877° SW	33.367°	2025-08-03 07:07:35.169Z	207.896° SW

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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Authenticating...

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Check out ARIANE 2 R/B, 19122 on other resources

View ARIANE 2 R/B, 19122 on Heavens-Above

View ARIANE 2 R/B, 19122 on Keep Track

View ARIANE 2 R/B, 19122 on Celestrak

View ARIANE 2 R/B, 19122 on Gunter's Space Page

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