RAY 1.0, 62627
Orbit data source: Space-Track
RAY 1.0, 62627 is a payload satellite owned by Inversion Space (US) in SSO that was launched on Tue, 14 Jan 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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62627 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Inversion Space
Mission
Operational Commercial Technology
Bus & Motor
RAY, Unknown motor
Mass
63 kg wet, 32 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + Cone, 0.7 m
Radar Cross Section
0.875 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 RAY 1.0
1 62627U 25009U 26305.77381837 .00002369 00000-0 10848-3 0 9993
2 62627 97.3880 21.5878 0009479 145.4363 214.7490 15.21425382 99598Epoch: 2026-11-01T18:34Z
TLE epoch observation values (Epoch: 2026-11-01T18:34:17.907Z)
Latitude
-0.00009°
Longitude
61.95283°
Altitude
509.995 km
Speed
7.606 km/s
True Right ascension
01h 26m 21s
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
19:33:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.022 km
Perigee altitude
491.985 km
Semi-major axis
6,876.64 km
Eccentricity
0.00095
Inclination
97.388°
RAAN
21.5878°
Arg. of periapsis
145.4363°
True anomaly
214.68715°
Mean anomaly
214.749°
Eccentric anomaly
214.71807°
Mean motion
3.80609 °/min
Orbital period
94.59 mins
BSTAR
0.00010848
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.RAY 1.0 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 | 2026-11-02 04:12:08.850Z | 99.537° ESE | 2026-11-02 04:14:08.850Z | 65.99° ENE | 14.439° | 2026-11-02 04:16:08.850Z | 33.092° NE |
| 4 mins | 2026-11-02 05:46:08.850Z | 218.369° SW | 2026-11-02 05:47:08.850Z | 246.736° WSW | 33.789° | 2026-11-02 05:50:08.850Z | 323.132° NNW |
| 4 mins | 2026-11-02 18:49:08.850Z | 331.361° NNW | 2026-11-02 18:51:08.850Z | 286.72° WNW | 23.766° | 2026-11-02 18:53:08.850Z | 244.702° WSW |
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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