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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 15 hours ago
TLE from 15 hours ago
0 SPACEEYE-T1
1 63229U 25052V 26032.68008625 .00005038 00000-0 23011-3 0 9990
2 63229 97.4125 287.3995 0003120 266.8620 93.2259 15.21026817 49232Epoch: 2026-02-01T16:19Z
TLE epoch observation values (Epoch: 2026-02-01T16:19:19.452Z)
Latitude
-0.00003°
Longitude
-89.31779°
Altitude
505.955 km
Speed
7.611 km/s
True Right ascension
19h 09m 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
08:48:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.853 km
Perigee altitude
497.561 km
Semi-major axis
6,877.844 km
Eccentricity
0.00031
Inclination
97.4125°
RAAN
287.3995°
Arg. of periapsis
266.862°
True anomaly
93.2616°
Mean anomaly
93.2259°
Eccentric anomaly
93.24375°
Mean motion
3.80509 °/min
Orbital period
94.61 mins
BSTAR
0.00023011
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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 | 2026-02-02 16:08:52.641Z | 120.242° SE | 2026-02-02 16:11:52.641Z | 61.706° ENE | 20.801° | 2026-02-02 16:13:52.641Z | 23.814° NE |
| 4 mins | 2026-02-02 17:43:52.641Z | 234.407° WSW | 2026-02-02 17:44:52.641Z | 255.636° W | 19.451° | 2026-02-02 17:47:52.641Z | 313.381° NW |
| 4 mins | 2026-02-03 05:13:52.641Z | 57.511° ENE | 2026-02-03 05:14:52.641Z | 85.788° E | 27.708° | 2026-02-03 05:17:52.641Z | 157.107° SSE |
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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