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: 8 hours ago
TLE from 8 hours ago
0 IOD1_STARTICAL
1 63212U 25052C 26175.18605358 .00055442 00000-0 84805-3 0 9993
2 63212 97.3815 77.0948 0004240 103.6927 256.4799 15.54200979 71576Epoch: 2026-06-24T04:27Z
TLE epoch observation values (Epoch: 2026-06-24T04:27:55.029Z)
Latitude
-0.00001°
Longitude
97.76863°
Altitude
408.287 km
Speed
7.665 km/s
True Right ascension
05h 08m 22s
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
23:31:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
404.27 km
Perigee altitude
398.521 km
Semi-major axis
6,779.533 km
Eccentricity
0.00042
Inclination
97.3815°
RAAN
77.0948°
Arg. of periapsis
103.6927°
True anomaly
256.43267°
Mean anomaly
256.4799°
Eccentric anomaly
256.45628°
Mean motion
3.88815 °/min
Orbital period
92.59 mins
BSTAR
0.00084805
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-24 16:58:10.423Z | 125.742° SE | 2026-06-24 17:00:10.423Z | 79.978° E | 23.04° | 2026-06-24 17:02:10.423Z | 24.815° NE |
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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