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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63212 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
GOMSpace
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 IOD1_STARTICAL
1 63212U 25052C 25269.25512323 .00039459 00000-0 13757-2 0 9990
2 63212 97.4093 162.6925 0003694 32.1621 327.9844 15.29519028 29848Epoch: 2025-09-26T06:07Z
TLE epoch observation values (Epoch: 2025-09-26T06:07:22.647Z)
Latitude
0°
Longitude
65.54361°
Altitude
478.205 km
Speed
7.628 km/s
True Right ascension
10h 50m 46s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:20:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.734 km
Perigee altitude
471.671 km
Semi-major axis
6,852.339 km
Eccentricity
0.00037
Inclination
97.4093°
RAAN
162.6925°
Arg. of periapsis
32.1621°
True anomaly
327.96195°
Mean anomaly
327.9844°
Eccentric anomaly
327.97318°
Mean motion
3.82635 °/min
Orbital period
94.08 mins
BSTAR
0.0013757
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Other satellites on launch #52 in the year 2025 (2025-03-15 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.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 | 2025-09-26 17:14:45.868Z | 182.596° SSW | 2025-09-26 17:16:45.868Z | 222.239° SW | 38.838° | 2025-09-26 17:19:45.868Z | 336.849° NNW |
| 5 mins | 2025-09-27 06:14:45.868Z | 347.126° N | 2025-09-27 06:16:45.868Z | 282.214° WNW | 34.455° | 2025-09-27 06:19:45.868Z | 215.129° SW |
| 5 mins | 2025-09-27 16:48:45.868Z | 143.368° SSE | 2025-09-27 16:50:45.868Z | 59.007° ENE | 38.87° | 2025-09-27 16:53:45.868Z | 358.071° N |
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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