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: 14 hours ago
TLE from 14 hours ago
0 SPACEEYE-T1
1 63229U 25052V 26083.32523451 .00005494 00000-0 24586-3 0 9990
2 63229 97.4043 337.2359 0006682 88.5370 271.6632 15.21670544 56931Epoch: 2026-03-24T07:48Z
TLE epoch observation values (Epoch: 2026-03-24T07:48:20.261Z)
Latitude
0.00002°
Longitude
38.34697°
Altitude
503.764 km
Speed
7.612 km/s
True Right ascension
22h 28m 56s
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
03:07:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.359 km
Perigee altitude
493.17 km
Semi-major axis
6,875.902 km
Eccentricity
0.00067
Inclination
97.4043°
RAAN
337.2359°
Arg. of periapsis
88.537°
True anomaly
271.58666°
Mean anomaly
271.6632°
Eccentric anomaly
271.62493°
Mean motion
3.8067 °/min
Orbital period
94.57 mins
BSTAR
0.00024586
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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 | 2026-03-25 04:54:16.653Z | 53.926° ENE | 2026-03-25 04:56:16.653Z | 91.712° ESE | 18.127° | 2026-03-25 04:58:16.653Z | 131.588° SE |
| 4 mins | 2026-03-25 06:28:16.653Z | 330.885° NNW | 2026-03-25 06:30:16.653Z | 285.057° WNW | 22.204° | 2026-03-25 06:32:16.653Z | 243.413° WSW |
| 5 mins | 2026-03-25 17:05:16.653Z | 182.191° SSW | 2026-03-25 17:07:16.653Z | 250.44° W | 42.159° | 2026-03-25 17:10:16.653Z | 340.068° N |
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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