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ION SCV-006, 52761

Orbit data source: Space-Track

ION SCV-006, 52761 is a payload satellite owned by D-ORBIT (IT) in SSO 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.

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Iframe URL

https://www.satcat.com/sats-embedded/52761?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

52761, 2022-057AF

Orbit

SSO

Country

IT

Related business

Manufacturer

D-ORBIT

Mission

Operational Commercial Technology

Bus & Motor

ION-SC, PM200

Mass

220 kg wet, 150 kg dry

Launch date (UTC)

2022-05-25 (4 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 0.2 m

Radar Cross Section

0.240 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago

0 ION SCV-006
1 52761U 22057AF  25348.91503643  .00009369  00000-0  23350-3 0  9993
2 52761  97.5849 124.6895 0020727  60.7873 299.5443 15.40234760197701

Epoch: 2025-12-14T21:57Z

TLE epoch observation values (Epoch: 2025-12-14T21:57:39.147Z)

Latitude

0.00005°

Longitude

71.45527°

Altitude

441.575 km

Speed

7.651 km/s

True Right ascension

08h 18m 45s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

13:22:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

456.499 km

Perigee altitude

428.226 km

Semi-major axis

6,820.5 km

Eccentricity

0.00207

Inclination

97.5849°

RAAN

124.6895°

Arg. of periapsis

60.7873°

True anomaly

299.33741°

Mean anomaly

299.5443°

Eccentric anomaly

299.44088°

Mean motion

3.85318 °/min

Orbital period

93.43 mins

BSTAR

0.0002335

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

NUSAT-31 (RUBY PAYNE-S), 52752

LEMUR 2 KAREN_B, 52736 (Decayed)

FOSSASAT2E8, 52779 (Decayed)

OP15 FLT2 (TYVAK-0821), 52735 (Decayed)

CNCE5, 52768 (Decayed)

CENTAURI 5 (TYVAK-0212), 52742 (Decayed)

NUSAT-30 (MARGHERITA), 52748 (Decayed)

FOSSASAT2E12, 52773 (Decayed)

PLANETUM1, 52738 (Decayed)

CONNECTA T1.1, 52739

NUSAT-28 (ALICE LEE), 52747

CNCE4, 52767 (Decayed)

LEMUR 2 TENNYSONLILY, 52732 (Decayed)

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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ION SCV-006 Visibility forecast

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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.
6 mins	2025-12-15 21:54:10.505Z	21.391° NNE	2025-12-15 21:57:10.505Z	97.622° ESE	40.078°	2025-12-15 22:00:10.505Z	179.709° S

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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 ION SCV-006, 52761 on other resources

View ION SCV-006, 52761 on NASA - NSSDCA Website

View ION SCV-006, 52761 on Heavens-Above

View ION SCV-006, 52761 on Keep Track

View ION SCV-006, 52761 on Celestrak

View ION SCV-006, 52761 on Gunter's Space Page

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

Documentation

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