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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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: 15 hours ago
TLE from 15 hours ago
0 IOD1_STARTICAL
1 63212U 25052C 26083.54700815 .00041916 00000-0 88798-3 0 9991
2 63212 97.3927 343.2608 0004056 77.4597 282.7106 15.44973488 57385Epoch: 2026-03-24T13:07Z
TLE epoch observation values (Epoch: 2026-03-24T13:07:41.504Z)
Latitude
0.00008°
Longitude
-35.68524°
Altitude
433.974 km
Speed
7.652 km/s
True Right ascension
22h 53m 02s
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
08:48:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.149 km
Perigee altitude
425.627 km
Semi-major axis
6,806.525 km
Eccentricity
0.00041
Inclination
97.3927°
RAAN
343.2608°
Arg. of periapsis
77.4597°
True anomaly
282.66526°
Mean anomaly
282.7106°
Eccentric anomaly
282.68793°
Mean motion
3.86505 °/min
Orbital period
93.14 mins
BSTAR
0.00088798
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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 | 2026-03-25 17:15:01.558Z | 161.009° S | 2026-03-25 17:17:01.558Z | 39.348° NE | 44.112° | 2026-03-25 17:20:01.558Z | 350.833° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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