TOMORROW-S6, 63225
Orbit data source: Space-Track
TOMORROW-S6, 63225 is a payload satellite owned by Tomorrow.io (US) 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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63225 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Blue Canyon
Mission
Operational Commercial Weather
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.138 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 TOMORROW-S6
1 63225U 25052R 26221.66204487 .00002462 00000-0 10820-3 0 9990
2 63225 97.3940 113.7378 0003882 326.5549 33.5442 15.22831224 77989Epoch: 2026-08-09T15:53Z
TLE epoch observation values (Epoch: 2026-08-09T15:53:20.676Z)
Latitude
-0.00005°
Longitude
-82.75417°
Altitude
498.175 km
Speed
7.617 km/s
True Right ascension
07h 34m 57s
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
16:41:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.935 km
Perigee altitude
491.599 km
Semi-major axis
6,872.404 km
Eccentricity
0.00039
Inclination
97.394°
RAAN
113.7378°
Arg. of periapsis
326.5549°
True anomaly
33.56879°
Mean anomaly
33.5442°
Eccentric anomaly
33.55649°
Mean motion
3.80961 °/min
Orbital period
94.5 mins
BSTAR
0.0001082
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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.TOMORROW-S6 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 | 2026-08-10 05:04:20.819Z | 39.227° NE | 2026-08-10 05:07:20.819Z | 96.578° ESE | 23.289° | 2026-08-10 05:10:20.819Z | 153.281° SSE |
| 4 mins | 2026-08-10 06:39:20.819Z | 321.489° NNW | 2026-08-10 06:40:20.819Z | 302.188° NW | 17.307° | 2026-08-10 06:43:20.819Z | 246.813° WSW |
| 6 mins | 2026-08-10 17:14:20.819Z | 186.368° SSW | 2026-08-10 17:17:20.819Z | 243.145° WSW | 35.551° | 2026-08-10 17:20:20.819Z | 331.331° 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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