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: 16 hours ago
TLE from 16 hours ago
0 SPACEEYE-T1
1 63229U 25052V 26192.71013942 .00002911 00000-0 12788-3 0 9995
2 63229 97.3926 84.8620 0006522 72.6994 287.4955 15.22695584 73579Epoch: 2026-07-11T17:02Z
TLE epoch observation values (Epoch: 2026-07-11T17:02:36.045Z)
Latitude
-0.00012°
Longitude
-100.40763°
Altitude
499.462 km
Speed
7.615 km/s
True Right ascension
05h 39m 26s
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
21:50:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.158 km
Perigee altitude
490.193 km
Semi-major axis
6,872.813 km
Eccentricity
0.00065
Inclination
97.3926°
RAAN
84.862°
Arg. of periapsis
72.6994°
True anomaly
287.4242°
Mean anomaly
287.4955°
Eccentric anomaly
287.45985°
Mean motion
3.80927 °/min
Orbital period
94.51 mins
BSTAR
0.00012788
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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 | 2026-07-12 16:49:47.030Z | 162.672° S | 2026-07-12 16:52:47.030Z | 41.074° NE | 44.309° | 2026-07-12 16:55:47.030Z | 350.917° N |
| 5 mins | 2026-07-13 05:53:47.030Z | 359.714° N | 2026-07-13 05:55:47.030Z | 264.033° W | 42.309° | 2026-07-13 05:58:47.030Z | 202.52° SW |
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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