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ICEYE-X14, 51070

Orbit data source: Space-Track

ICEYE-X14, 51070 is a payload satellite owned by ICEYE US (US) in SSO that was launched on Thu, 13 Jan 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/51070?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

51070, 2022-002CQ

Orbit

SSO

Country

US

Related business

Manufacturer

ICEYE US

Mission

Operational Commercial Radar Imaging

Bus & Motor

ICEYE, Unknown motor

Mass

80 kg wet, 80 kg dry

Launch date (UTC)

2022-01-13 (4 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 1 Pan, 1.6 m

Radar Cross Section

1.837 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 ICEYE-X14
1 51070U 22002CQ  25345.28199458  .00674044  00000-0  31673-2 0  9991
2 51070  97.3158  60.0239 0002967 328.9202  31.1891 15.81418752217755

Epoch: 2025-12-11T06:46Z

TLE epoch observation values (Epoch: 2025-12-11T06:46:04.331Z)

Latitude

0.00001°

Longitude

-121.73436°

Altitude

327.901 km

Speed

7.713 km/s

True Right ascension

04h 00m 05s

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

13:02:19

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

325.297 km

Perigee altitude

321.32 km

Semi-major axis

6,701.445 km

Eccentricity

0.0003

Inclination

97.3158°

RAAN

60.0239°

Arg. of periapsis

328.9202°

True anomaly

31.20671°

Mean anomaly

31.1891°

Eccentric anomaly

31.19791°

Mean motion

3.95631 °/min

Orbital period

90.99 mins

BSTAR

0.0031673

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Other satellites on launch #2 in the year 2022 (2022-01-13 UTC)

FOSSASAT2E1, 50985 (Decayed)

OBJECT DD, 51083 (Decayed)

TEVEL 4, 51063 (Decayed)

FLOCK 4X 32, 51024 (Decayed)

LEMUR 2 DJIRANG, 51058 (Decayed)

STORK-1, 51087 (Decayed)

FLOCK 4X 17, 51035 (Decayed)

USA 322, 51078 (Decayed)

DODONA, 51084 (Decayed)

FLOCK 4X 25, 51016 (Decayed)

FLOCK 4X 13, 51028 (Decayed)

OBJECT CW, 51076 (Decayed)

LABSAT, 51086 (Decayed)

LEMUR 2 ROHOVITHSA, 51036 (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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ICEYE-X14 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.
4 mins	2025-12-11 17:57:32.261Z	19.802° NNE	2025-12-11 17:59:32.261Z	158.291° S	40.007°	2025-12-11 18:01:32.261Z	185.92° SSW

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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 ICEYE-X14, 51070 on other resources

View ICEYE-X14, 51070 on NASA - NSSDCA Website

View ICEYE-X14, 51070 on Heavens-Above

View ICEYE-X14, 51070 on Keep Track

View ICEYE-X14, 51070 on Celestrak

View ICEYE-X14, 51070 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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