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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Edit Public Description
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, 0.6 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 RAY 1.0
1 62627U 25009U 26035.26424718 .00004295 00000-0 20375-3 0 9999
2 62627 97.4100 116.0222 0009534 29.9730 330.2049 15.19765895 58483Epoch: 2026-02-04T06:20Z
TLE epoch observation values (Epoch: 2026-02-04T06:20:30.956Z)
Latitude
-0.00002°
Longitude
-113.5401°
Altitude
503.942 km
Speed
7.615 km/s
True Right ascension
07h 44m 05s
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
01:22:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.075 km
Perigee altitude
496.953 km
Semi-major axis
6,881.651 km
Eccentricity
0.00095
Inclination
97.41°
RAAN
116.0222°
Arg. of periapsis
29.973°
True anomaly
330.15056°
Mean anomaly
330.2049°
Eccentric anomaly
330.17773°
Mean motion
3.80193 °/min
Orbital period
94.69 mins
BSTAR
0.00020375
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-05 04:36:14.580Z | 124.002° SE | 2026-02-05 04:39:14.580Z | 64.959° ENE | 22.332° | 2026-02-05 04:41:14.580Z | 23.869° NE |
| 4 mins | 2026-02-05 06:11:14.580Z | 232.424° WSW | 2026-02-05 06:13:14.580Z | 273.818° WNW | 17.867° | 2026-02-05 06:15:14.580Z | 309.134° NW |
| 5 mins | 2026-02-05 17:41:14.580Z | 41.482° NE | 2026-02-05 17:43:14.580Z | 94.033° ESE | 30.692° | 2026-02-05 17:46:14.580Z | 162.768° S |
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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