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IOD1_STARTICAL, 63212

Orbit data source: Space-Track

IOD1_STARTICAL, 63212 is a Spanish payload satellite in SSO that was launched on Sat, 15 Mar 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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/63212?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63212, 2025-052C

Orbit

SSO

Country

ES / SPN

Related business

Startical S.L. (Unknown / E)

Manufacturer

GOMSpace

Mission

Operational Commercial Communications

Bus & Motor

CUBESAT 16U, Unknown motor

Mass

20 kg wet, 20 kg dry

Launch date (UTC)

2025-03-15 (1 year ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan + 1 Ant, 0.3 m

Radar Cross Section

0.152 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 IOD1_STARTICAL
1 63212U 25052C   26129.65649800  .00034907  00000-0  63474-3 0  9996
2 63212  97.3882  30.3382 0001989 138.9636 221.1766 15.49454042 64514

Epoch: 2026-05-09T15:45Z

TLE epoch observation values (Epoch: 2026-05-09T15:45:21.427Z)

Latitude

0.00009°

Longitude

-73.47189°

Altitude

422.471 km

Speed

7.657 km/s

True Right ascension

02h 01m 21s

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

11:58:07

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

416.599 km

Perigee altitude

413.897 km

Semi-major axis

6,793.385 km

Eccentricity

0.0002

Inclination

97.3882°

RAAN

30.3382°

Arg. of periapsis

138.9636°

True anomaly

221.1616°

Mean anomaly

221.1766°

Eccentric anomaly

221.1691°

Mean motion

3.87627 °/min

Orbital period

92.87 mins

BSTAR

0.00063474

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Other satellites on launch #52 in the year 2025 (2025-03-15 UTC)

LEMUR 2 DELOITTE-1, 63259

UNICORN-2P, 63981 (Decayed)

UNICORN-2Q, 63491 (Decayed)

OBJECT BJ, 63396 (Decayed)

PIONEER-03, 63224 (Decayed)

UNICORN-2O, 63980 (Decayed)

OBJECT D, 63213

TOMORROW-S6, 63225

BUCCANEER MM, 63245

LEMUR 2 LEIA-PHILIP, 63246

LEMUR 2 THEFALCONER, 63264

HADES-ICM, 63492

UVSQ-SAT NG, 63251

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

IOD1_STARTICAL 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.
5 mins	2026-05-10 06:15:44.747Z	10.662° NNE	2026-05-10 06:18:44.747Z	202.82° SW	42.359°	2026-05-10 06:20:44.747Z	194.685° 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 IOD1_STARTICAL, 63212 on other resources

View IOD1_STARTICAL, 63212 on NASA - NSSDCA Website

View IOD1_STARTICAL, 63212 on Heavens-Above

View IOD1_STARTICAL, 63212 on Keep Track

View IOD1_STARTICAL, 63212 on Celestrak

View IOD1_STARTICAL, 63212 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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