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: 11 hours ago
TLE from 11 hours ago
0 SPACEEYE-T1
1 63229U 25052V 26129.67767741 .00003337 00000-0 14858-3 0 9996
2 63229 97.3990 22.8434 0003093 296.0948 63.9970 15.22146843 63983Epoch: 2026-05-09T16:15Z
TLE epoch observation values (Epoch: 2026-05-09T16:15:51.328Z)
Latitude
0.00001°
Longitude
-88.61214°
Altitude
501.527 km
Speed
7.614 km/s
True Right ascension
01h 31m 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
11:14:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.455 km
Perigee altitude
494.203 km
Semi-major axis
6,874.466 km
Eccentricity
0.00031
Inclination
97.399°
RAAN
22.8434°
Arg. of periapsis
296.0948°
True anomaly
64.02886°
Mean anomaly
63.997°
Eccentric anomaly
64.01293°
Mean motion
3.80789 °/min
Orbital period
94.54 mins
BSTAR
0.00014858
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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 | 2026-05-10 05:27:28.234Z | 27.143° NE | 2026-05-10 05:30:28.234Z | 127.441° SE | 36.905° | 2026-05-10 05:33:28.234Z | 176.992° S |
| 4 mins | 2026-05-10 16:05:28.234Z | 103.386° ESE | 2026-05-10 16:07:28.234Z | 60.527° ENE | 18.862° | 2026-05-10 16:09:28.234Z | 24.779° NE |
| 4 mins | 2026-05-10 17:39:28.234Z | 234.806° WSW | 2026-05-10 17:40:28.234Z | 258.497° W | 21.413° | 2026-05-10 17:43:28.234Z | 317.067° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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