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
0.875 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 RAY 1.0
1 62627U 25009U 25340.46797231 .00006710 00000-0 32211-3 0 9998
2 62627 97.4186 57.3009 0007851 222.5190 137.5438 15.19162301 49403Epoch: 2025-12-06T11:13Z
TLE epoch observation values (Epoch: 2025-12-06T11:13:52.807Z)
Latitude
0.00003°
Longitude
173.33558°
Altitude
515.452 km
Speed
7.604 km/s
True Right ascension
03h 49m 12s
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
20:43:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.743 km
Perigee altitude
499.934 km
Semi-major axis
6,883.476 km
Eccentricity
0.00079
Inclination
97.4186°
RAAN
57.3009°
Arg. of periapsis
222.519°
True anomaly
137.60449°
Mean anomaly
137.5438°
Eccentric anomaly
137.57415°
Mean motion
3.80042 °/min
Orbital period
94.73 mins
BSTAR
0.00032211
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-07 04:45:35.468Z | 129.961° SE | 2025-12-07 04:48:35.468Z | 61.748° ENE | 27.136° | 2025-12-07 04:51:35.468Z | 9.028° NNE |
| 5 mins | 2025-12-07 17:50:35.468Z | 30.792° NE | 2025-12-07 17:52:35.468Z | 76.115° E | 35.372° | 2025-12-07 17:55:35.468Z | 169.316° 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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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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