INTELSAT 29E DEB, 62723

Orbit data source: Space-Track

INTELSAT 29E DEB, 62723 is space debris in GEO originally from a launch on Wed, 27 Jan 2016 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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/62723?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/62723?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

62723, 2016-004E

Orbit

GEO

Last TLE update

3 months ago

Origin

ArianeGroup (Unknown / ITSO)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2016-01-27 (9 years ago)

Launch vehicle

Unknown

Launch site

French Guiana (FRGUI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

RCS unknown

Expand to show TLE details & history

TLE from 3 months ago

0 INTELSAT 29E DEB
1 62723U 16004E   25086.52352323  .00000010  00000-0  00000-0 0  9998
2 62723   5.4043  75.8258 0623060 307.4539  47.2101  1.00540659  8060

Epoch: 2025-03-27T12:33Z

TLE epoch observation values (Epoch: 2025-03-27T12:33:52.407Z)

Latitude

-0.00089°

Longitude

62.38968°

Altitude

34,024.021 km

Speed

3.203 km/s

True Right ascension

05h 04m 12s

True Declination

0° 00' 03"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-4.36958°

Longitude

-68.78878°

Altitude

35,114.04 km

Speed

3.122 km/s

Apparent Right ascension

19h 55m 53s

Apparent Declination

-9° 25' 05"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

03:54:47

Azimuth

282.399° WNW

Elevation

-28.695°

Doppler factor

Orbital elements

Apogee altitude

38,334.948 km

Perigee altitude

33,089.956 km

Semi-major axis

42,090.589 km

Eccentricity

0.06231

Inclination

5.4043°

RAAN

75.8258°

Arg. of periapsis

307.4539°

True anomaly

Unknown

Mean anomaly

47.2101°

Eccentric anomaly

Unknown

Mean motion

0.25134 °/min

Orbital period

1,432.31 mins

BSTAR

Loading historical data...

62723 neighbors

Authenticating...

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Other satellites on launch #4 in the year 2016 (2016-01-27 UTC)

INTELSAT 29E, 41308

ARIANE 5 R/B, 41309

ARIANE 5 DEB, 44602 (Decayed)

INTELSAT 29E DEB, 45488

INTELSAT 29E DEB Visibility

Observer location: undefined°, undefined°

INTELSAT 29E DEB is likely not visible in the next few days

Authenticating...

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Check out INTELSAT 29E DEB, 62723 on other resources

View INTELSAT 29E DEB, 62723 on Heavens-Above

View INTELSAT 29E DEB, 62723 on Keep Track

View INTELSAT 29E DEB, 62723 on Celestrak

View INTELSAT 29E DEB, 62723 on Gunter's Space Page

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