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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 5 hours ago
TLE from 5 hours ago
0 SPACEEYE-T1
1 63229U 25052V 25301.65075207 .00008011 00000-0 38009-3 0 9992
2 63229 97.4160 192.9645 0003351 229.5871 130.5072 15.19525298 34645Epoch: 2025-10-28T15:37Z
TLE epoch observation values (Epoch: 2025-10-28T15:37:04.978Z)
Latitude
-0.00003°
Longitude
-78.54143°
Altitude
511.863 km
Speed
7.607 km/s
True Right ascension
12h 51m 51s
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
15:51:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.547 km
Perigee altitude
501.935 km
Semi-major axis
6,882.378 km
Eccentricity
0.00034
Inclination
97.416°
RAAN
192.9645°
Arg. of periapsis
229.5871°
True anomaly
130.53639°
Mean anomaly
130.5072°
Eccentric anomaly
130.52179°
Mean motion
3.80133 °/min
Orbital period
94.7 mins
BSTAR
0.00038009
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-29 06:25:20.343Z | 326.275° NNW | 2025-10-29 06:26:20.343Z | 301.934° NW | 24.414° | 2025-10-29 06:29:20.343Z | 234.875° WSW |
| 6 mins | 2025-10-29 17:02:20.343Z | 175.307° S | 2025-10-29 17:04:20.343Z | 201.07° SSW | 41.402° | 2025-10-29 17:08:20.343Z | 344.038° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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