DECAYED

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CLUSTER II-FM6, 26411 (Decayed)

Orbit data source: Space-Track

CLUSTER II-FM6, 26411 was a payload satellite owned by ESA (ESA) in HEO that was launched on Sun, 16 Jul 2000 UTC via a SOYUZ-U-PVB launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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.

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<iframe src="https://www.satcat.com/sats-embedded/26411?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/26411?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26411, 2000-041B

Orbit

Decayed

Last TLE update

11 months ago

Origin

European Space Agency (ESA)

Manufacturer

Astrium-Frh.

Mission

Decayed Civil Science

Bus & Motor

CLUSTER, S400

Mass

1,186 kg wet, 550 kg dry

Launch date (UTC)

2000-07-16 (25 years ago)

Launch vehicle

SOYUZ-U-PVB

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 4 Ant, 50.0 m

Radar Cross Section

31.548 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 11 months ago

0 CLUSTER II-FM6
1 26411U 00041B   24252.84968039  .00055456 -32455-3  00000+0 0  9998
2 26411 150.0716  39.2522 9137804 255.7707   0.1507  0.44420051 28489

Epoch: 2024-09-08T20:23Z

TLE epoch observation values (Epoch: 2024-09-08T20:23:32.385Z)

Latitude

-28.16673°

Longitude

-142.17872°

Altitude

73.096 km

Speed

10.87 km/s

True Right ascension

10h 08m 22s

True Declination

-28° 00' 31"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

132,491.982 km

Perigee altitude

-121.763 km

Semi-major axis

72,563.247 km

Eccentricity

0.91378

Inclination

150.0716°

RAAN

39.2522°

Arg. of periapsis

255.7707°

True anomaly

8.20778°

Mean anomaly

0.1507°

Eccentric anomaly

1.74499°

Mean motion

0.11104 °/min

Orbital period

3,242.16 mins

BSTAR

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Other satellites on launch #41 in the year 2000 (2000-07-16 UTC)

CLUSTER II-FM7, 26410

FREGAT R/B, 26412 (Decayed)

CLUSTER II-FM6 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.
197 mins	2025-08-02 09:31:43.900Z	241.538° WSW	2025-08-02 09:31:43.900Z	241.538° WSW	37.273°	2025-08-02 12:48:43.900Z	279.207° WNW
507 mins	2025-08-03 01:04:43.900Z	85.503° E	2025-08-03 06:01:43.900Z	175.692° S	40.096°	2025-08-03 09:31:43.900Z	253.883° W

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 CLUSTER II-FM6, 26411 (Decayed) on other resources

View CLUSTER II-FM6, 26411 (Decayed) on Celestrak

View CLUSTER II-FM6, 26411 (Decayed) on Gunter's Space Page

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