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, 4.0 m
Radar Cross Section
7.637 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 SPACEEYE-T1
1 63229U 25052V 26265.44443759 .00003090 00000-0 13357-3 0 9991
2 63229 97.3800 156.3982 0005298 149.6141 210.5404 15.23205531 84640Epoch: 2026-09-22T10:39Z
TLE epoch observation values (Epoch: 2026-09-22T10:39:59.407Z)
Latitude
-0.00003°
Longitude
-4.90915°
Altitude
502.413 km
Speed
7.611 km/s
True Right ascension
10h 25m 35s
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
13:42:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.78 km
Perigee altitude
489.499 km
Semi-major axis
6,871.277 km
Eccentricity
0.00053
Inclination
97.38°
RAAN
156.3982°
Arg. of periapsis
149.6141°
True anomaly
210.50957°
Mean anomaly
210.5404°
Eccentric anomaly
210.52498°
Mean motion
3.81054 °/min
Orbital period
94.47 mins
BSTAR
0.00013357
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-23 06:09:39.120Z | 342.442° N | 2026-09-23 06:11:39.120Z | 280.984° WNW | 38.807° | 2026-09-23 06:14:39.120Z | 218.81° SW |
| 5 mins | 2026-09-23 16:45:39.120Z | 156.339° SSE | 2026-09-23 16:47:39.120Z | 116.424° SE | 64.272° | 2026-09-23 16:50:39.120Z | 355.121° 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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