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TURKMENALEM 52E/MONACOSA, 40617

Orbit data source: Space-Track

TURKMENALEM 52E/MONACOSA, 40617 is a TM and MC payload satellite in GEO that was launched on Mon, 27 Apr 2015 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days

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Iframe URL

https://www.satcat.com/sats-embedded/40617?theme=dark&initialShowStats=false

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Identifier

40617, 2015-023A

Orbit

GEO

Country

Unknown / TMMC

Related business

Space Systems International - Monaco S.A.M. (MC)

Manufacturer

Thales Alenia

Mission

Operational Commercial Communications

Bus & Motor

SPACEBUS 4000C2, S400

Mass

4,700 kg wet, 1,823 kg dry

Launch date (UTC)

2015-04-27 (11 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 15.0 m

Radar Cross Section

26.037 m², Large (>1 m²)

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Last TLE update: 10 hours ago

TLE from 10 hours ago

0 TURKMENALEM 52E/MONACOSA
1 40617U 15023A   26062.10530860  .00000088  00000-0  00000+0 0  9993
2 40617   0.0126 128.9368 0002895 222.1718 259.6849  1.00273880 39782

Epoch: 2026-03-03T02:31Z

TLE epoch observation values (Epoch: 2026-03-03T02:31:38.663Z)

Latitude

0.03479°

Longitude

51.99632°

Altitude

35,787.656 km

Speed

3.075 km/s

True Right ascension

16h 43m 11s

True Declination

0° 02' 05"

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

16:44:41

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,799.285 km

Perigee altitude

35,774.871 km

Semi-major axis

42,165.215 km

Eccentricity

0.00029

Inclination

0.0126°

RAAN

128.9368°

Arg. of periapsis

222.1718°

True anomaly

259.65226°

Mean anomaly

259.6849°

Eccentric anomaly

259.66858°

Mean motion

0.25068 °/min

Orbital period

1,436.12 mins

BSTAR

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Other satellites on launch #23 in the year 2015 (2015-04-27 UTC)

FALCON 9 R/B, 40618

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TURKMENALEM 52E/MONACOSA Visibility

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TURKMENALEM 52E/MONACOSA is likely not visible in the next few days.

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40617 neighbors

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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 TURKMENALEM 52E/MONACOSA, 40617 on other resources

View TURKMENALEM 52E/MONACOSA, 40617 on NASA - NSSDCA Website

View TURKMENALEM 52E/MONACOSA, 40617 on Heavens-Above

View TURKMENALEM 52E/MONACOSA, 40617 on Keep Track

View TURKMENALEM 52E/MONACOSA, 40617 on Celestrak

View TURKMENALEM 52E/MONACOSA, 40617 on Gunter's Space Page

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

TURKMENALEM 52E/MONACOSA, 40617

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-03-03T02:31:38.663Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #23 in the year 2015 (2015-04-27 UTC)

TURKMENALEM 52E/MONACOSA Visibility

40617 neighbors

Co-orbital & Co-planar RSOs

Check out TURKMENALEM 52E/MONACOSA, 40617 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago