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 26219.96918850 .00047656 00000-0 56898-3 0 9991
2 63212 97.3733 123.4415 0003680 147.5434 212.6050 15.60897449 78546Epoch: 2026-08-07T23:15Z
TLE epoch observation values (Epoch: 2026-08-07T23:15:37.886Z)
Latitude
-0.00004°
Longitude
178.04638°
Altitude
390.307 km
Speed
7.675 km/s
True Right ascension
08h 13m 45s
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
21:50:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
384.461 km
Perigee altitude
379.486 km
Semi-major axis
6,760.111 km
Eccentricity
0.00037
Inclination
97.3733°
RAAN
123.4415°
Arg. of periapsis
147.5434°
True anomaly
212.58229°
Mean anomaly
212.605°
Eccentric anomaly
212.59364°
Mean motion
3.90492 °/min
Orbital period
92.19 mins
BSTAR
0.00056898
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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 | 2026-08-08 17:51:33.250Z | 181.962° SSW | 2026-08-08 17:53:33.250Z | 252.944° W | 40.797° | 2026-08-08 17:55:33.250Z | 335.754° NNW |
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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