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ICEYE-X13, 48916

Orbit data source: Space-Track

ICEYE-X13, 48916 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Wed, 30 Jun 2021 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/48916?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/48916?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

48916, 2021-059AP

Orbit

SSO

Country

FI / FIN

Related business

Manufacturer

ICEYE

Mission

Operational Commercial Radar Imaging

Bus & Motor

ICEYE, Unknown motor

Mass

80 kg wet, 80 kg dry

Launch date (UTC)

2021-06-30 (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-X13
1 48916U 21059AP  25308.95291941  .00247220  00000-0  90942-3 0  9997
2 48916  97.6388 125.5145 0001664 193.8053 166.3172 15.87641297242958

Epoch: 2025-11-04T22:52Z

TLE epoch observation values (Epoch: 2025-11-04T22:52:12.237Z)

Latitude

-0.00006°

Longitude

98.03097°

Altitude

313.154 km

Speed

7.72 km/s

True Right ascension

08h 22m 03s

True Declination

0° 00' 00"

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

03:12:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

306.897 km

Perigee altitude

304.672 km

Semi-major axis

6,683.921 km

Eccentricity

0.00017

Inclination

97.6388°

RAAN

125.5145°

Arg. of periapsis

193.8053°

True anomaly

166.32171°

Mean anomaly

166.3172°

Eccentric anomaly

166.31945°

Mean motion

3.97188 °/min

Orbital period

90.64 mins

BSTAR

0.00090942

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Other satellites on launch #59 in the year 2021 (2021-06-30 UTC)

SHANNON, 48938 (Decayed)

ICEYE-X12, 48914 (Decayed)

MANDRAKE 2 BAKER, 48908

SHERPA-FX2/TAGSAT-2, 48958

SPACEBEE-100, 48883 (Decayed)

DEMO8(TENZING), 48951

NUSAT-22 (SOFYA), 48919 (Decayed)

ICEYE-X11, 48918

ICEYE-X15, 48917 (Decayed)

ION SCV-003, 48912 (Decayed)

SPACEBEE-88, 48935 (Decayed)

YAM-2, 48911 (Decayed)

LEMUR 2 ANNABANANA, 48923 (Decayed)

SPACEBEE-107, 48894 (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.

Click here to try in Sandbox

ICEYE-X13 Visibility

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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.
ICEYE-X13 is likely not visible in the next few days.

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-X13, 48916 on other resources

View ICEYE-X13, 48916 on NASA - NSSDCA Website

View ICEYE-X13, 48916 on Heavens-Above

View ICEYE-X13, 48916 on Keep Track

View ICEYE-X13, 48916 on Celestrak

View ICEYE-X13, 48916 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

Go to standalone docs website

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