SPACEEYE-T1, 63229
Orbit data source: Space-Track
SPACEEYE-T1, 63229 is a payload satellite owned by SatRec Initiative (KR) 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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63229 intel report (Beta)
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Identifier
Orbit
Country
KR / SKORRelated business
Manufacturer
SatRec Initiative
Mission
Operational Commercial Imaging
Bus & Motor
SPACEEYE-T, Unknown motor
Mass
700 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 2.7 m
Radar Cross Section
7.637 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 SPACEEYE-T1
1 63229U 25052V 26220.44010233 .00002269 00000-0 99737-4 0 9993
2 63229 97.3879 112.1416 0004115 351.0201 9.0962 15.22902373 77796Epoch: 2026-08-08T10:33Z
TLE epoch observation values (Epoch: 2026-08-08T10:33:44.841Z)
Latitude
0.00004°
Longitude
-3.24666°
Altitude
497.392 km
Speed
7.617 km/s
True Right ascension
07h 28m 33s
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
07:24:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.881 km
Perigee altitude
491.225 km
Semi-major axis
6,872.19 km
Eccentricity
0.00041
Inclination
97.3879°
RAAN
112.1416°
Arg. of periapsis
351.0201°
True anomaly
9.10366°
Mean anomaly
9.0962°
Eccentric anomaly
9.09993°
Mean motion
3.80979 °/min
Orbital period
94.49 mins
BSTAR
0.000099737
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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.SPACEEYE-T1 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-09 06:02:29.089Z | 358.186° N | 2026-08-09 06:05:29.089Z | 291.625° WNW | 36.47° | 2026-08-09 06:08:29.089Z | 214.019° SW |
| 5 mins | 2026-08-09 16:40:29.089Z | 142.938° SSE | 2026-08-09 16:42:29.089Z | 52.264° ENE | 39.131° | 2026-08-09 16:45:29.089Z | 357.559° 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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