DECAYED

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CNCE4, 52767 (Decayed)

Orbit data source: Space-Track

CNCE4, 52767 was a payload satellite owned by MDA (US) in LEO that was launched on Wed, 25 May 2022 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

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/52767?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/52767?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

52767, 2022-057AM

Orbit

Decayed

Last TLE update

1 year ago

Origin

Missile Defense Agency (US)

Manufacturer

AFRL?

Mission

Decayed Defense Communications

Bus & Motor

CUBESAT 3U, Unknown motor

Mass

4 kg wet, 4 kg dry

Launch date (UTC)

2022-05-25 (3 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 0.3 m

Radar Cross Section

0.035 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 year ago

0 CNCE4
1 52767U 22057AM  24109.88813878  .10686156  26072-5  11827-2 0  9996
2 52767  97.5206 246.2159 0012945 266.9407  93.0409 16.36988063106239

Epoch: 2024-04-18T21:18Z

Definitive object data (Epoch: 2024-04-18T21:18:55.19Z)

Latitude

-0.00005°

Longitude

79.00801°

Altitude

177.532 km

Speed

7.799 km/s

True Right ascension

16h 24m 51s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at TLE epoch

Visualization observer readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

179.121 km

Perigee altitude

162.167 km

Semi-major axis

6,548.781 km

Eccentricity

0.0012945

Inclination

97.5206°

RAAN

246.2159°

Arg. of periapsis

266.9407°

True anomaly

93.18902°

Mean anomaly

93.0409°

Eccentric anomaly

93.11496°

Mean motion

4.09546 °/min

BSTAR

0.0011827

Orbital period

87.9 mins

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Other satellites on launch #57 in the year 2022 (2022-05-25 UTC)

LEMUR 2 TENNYSONLILY, 52732 (Decayed)

HAWK-5B, 52756

HAWK-5A, 52757

ICEYE-X19, 52758 (Decayed)

NUSAT-29 (EDITH CLARKE), 52764

ARMSAT1 URDANETA, 52765

CELESTIS 21/VARISAT 1C, 52766

CNCE5, 52768 (Decayed)

LEMUR 2 MIMI1307, 52769 (Decayed)

CNCE4 Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed

Authenticating...

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Check out CNCE4, 52767 (Decayed) on other resources

View CNCE4, 52767 (Decayed) on Celestrak

View CNCE4, 52767 (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.