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 26175.16335511 .00004020 00000-0 17625-3 0 9992
2 63229 97.3949 67.5972 0006397 117.1093 243.0796 15.22535188 70905Epoch: 2026-06-24T03:55Z
TLE epoch observation values (Epoch: 2026-06-24T03:55:13.881Z)
Latitude
-0.0001°
Longitude
96.46486°
Altitude
503.285 km
Speed
7.612 km/s
True Right ascension
04h 30m 23s
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
21:55:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.556 km
Perigee altitude
490.762 km
Semi-major axis
6,873.296 km
Eccentricity
0.00064
Inclination
97.3949°
RAAN
67.5972°
Arg. of periapsis
117.1093°
True anomaly
243.01426°
Mean anomaly
243.0796°
Eccentric anomaly
243.04693°
Mean motion
3.80887 °/min
Orbital period
94.52 mins
BSTAR
0.00017625
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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 | 2026-06-24 16:40:09.132Z | 152.239° SSE | 2026-06-24 16:43:09.132Z | 68.931° E | 40.221° | 2026-06-24 16:46:09.132Z | 357.951° N |
| 5 mins | 2026-06-25 05:44:09.132Z | 12.52° NNE | 2026-06-25 05:46:09.132Z | 161.011° S | 44.99° | 2026-06-25 05:49:09.132Z | 192.593° SSW |
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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