ARIANE 44L+3 DEB (SPELDA, 23867

Orbit data source: Space-Track

ARIANE 44L+3 DEB (SPELDA, 23867 is space debris in HEO originally from a launch on Thu, 16 May 1996 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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https://www.satcat.com/sats-embedded/23867?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

23867, 1996-030D

Orbit

HEO

Last TLE update

16 hours ago

Origin

ArianeGroup (FR)

Manufacturer

MMS/Stevenage

Mission

Spacecraft

Bus & Motor

SPELDA, Unknown motor

Mass

370 kg wet, 370 kg dry

Launch date (UTC)

1996-05-16 (29 years ago)

Launch vehicle

Unknown

Launch site

French Guiana (FRGUI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + Trunc Cone, 2.0 m

Radar Cross Section

15.080 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 16 hours ago

0 ARIANE 44L+3 DEB (SPELDA
1 23867U 96030D   25200.70984247  .00008722  00000-0  52729-2 0  9990
2 23867   3.7616 116.2612 6614797  33.9990 354.4280  3.11525032288357

Epoch: 2025-07-19T17:02Z

TLE epoch observation values (Epoch: 2025-07-19T17:02:10.389Z)

Latitude

-0.00013°

Longitude

-77.13916°

Altitude

812.261 km

Speed

9.525 km/s

True Right ascension

07h 44m 35s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

2.68125°

Longitude

57.19942°

Altitude

6,170.556 km

Speed

6.587 km/s

Apparent Right ascension

15h 11m 56s

Apparent Declination

-15° 29' 49"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:58:38

Azimuth

265.168° W

Elevation

-18.725°

Doppler factor

Orbital elements

Apogee altitude

26,533.544 km

Perigee altitude

327.495 km

Semi-major axis

19,808.657 km

Eccentricity

0.66148

Inclination

3.7616°

RAAN

116.2612°

Arg. of periapsis

33.999°

True anomaly

325.30593°

Mean anomaly

354.428°

Eccentric anomaly

343.94878°

Mean motion

0.7785 °/min

Orbital period

462.43 mins

BSTAR

0.0052729

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Other satellites on launch #30 in the year 1996 (1996-05-16 UTC)

PALAPA C2, 23864

INTELSAT 24 (AMOS 1), 23865

ARIANE 44L+3 R/B, 23866

ARIANE 44L+3 DEB (SPELDA 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.
363 mins	2025-07-20 09:49:30.340Z	245.294° WSW	2025-07-20 11:22:30.340Z	238.112° WSW	18.347°	2025-07-20 15:52:30.340Z	188.726° SSW
30 mins	2025-07-21 08:35:30.340Z	241.126° WSW	2025-07-21 09:05:30.340Z	231.547° WSW	20.443°	2025-07-21 09:05:30.340Z	231.547° WSW

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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Check out ARIANE 44L+3 DEB (SPELDA, 23867 on other resources

View ARIANE 44L+3 DEB (SPELDA, 23867 on Heavens-Above

View ARIANE 44L+3 DEB (SPELDA, 23867 on Keep Track

View ARIANE 44L+3 DEB (SPELDA, 23867 on Celestrak

View ARIANE 44L+3 DEB (SPELDA, 23867 on Gunter's Space Page

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