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 26256.24493395 .00002199 00000-0 10168-3 0 9999
2 62627 97.3929 332.9774 0007809 338.0788 22.0113 15.21182068 92060Epoch: 2026-09-13T05:52Z
TLE epoch observation values (Epoch: 2026-09-13T05:52:42.293Z)
Latitude
0.00003°
Longitude
-107.44118°
Altitude
500.384 km
Speed
7.617 km/s
True Right ascension
22h 11m 54s
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
03:33:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.608 km
Perigee altitude
493.867 km
Semi-major axis
6,877.375 km
Eccentricity
0.00078
Inclination
97.3929°
RAAN
332.9774°
Arg. of periapsis
338.0788°
True anomaly
22.04487°
Mean anomaly
22.0113°
Eccentric anomaly
22.02808°
Mean motion
3.80548 °/min
Orbital period
94.6 mins
BSTAR
0.00010168
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-13 17:29:41.201Z | 35.433° NE | 2026-09-13 17:32:41.201Z | 92.574° ESE | 29.798° | 2026-09-13 17:35:41.201Z | 156.026° SSE |
| 5 mins | 2026-09-14 05:41:41.201Z | 200.932° SSW | 2026-09-14 05:43:41.201Z | 253.281° W | 39.484° | 2026-09-14 05:46:41.201Z | 328.219° NNW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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