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: 17 hours ago
TLE from 17 hours ago
0 TOMORROW-S6
1 63225U 25052R 26083.49140008 .00004851 00000-0 21751-3 0 9994
2 63225 97.4099 337.6950 0007098 76.0566 284.1459 15.21664370 56969Epoch: 2026-03-24T11:47Z
TLE epoch observation values (Epoch: 2026-03-24T11:47:36.966Z)
Latitude
-0.00005°
Longitude
-21.17731°
Altitude
502.722 km
Speed
7.614 km/s
True Right ascension
22h 30m 46s
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
10:19:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.664 km
Perigee altitude
492.903 km
Semi-major axis
6,875.921 km
Eccentricity
0.00071
Inclination
97.4099°
RAAN
337.695°
Arg. of periapsis
76.0566°
True anomaly
284.06701°
Mean anomaly
284.1459°
Eccentric anomaly
284.10646°
Mean motion
3.80668 °/min
Orbital period
94.57 mins
BSTAR
0.00021751
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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 | 2026-03-25 05:42:36.590Z | 13.512° NNE | 2026-03-25 05:45:36.590Z | 31.55° NE | 43.577° | 2026-03-25 05:48:36.590Z | 190.047° SSW |
| 4 mins | 2026-03-25 16:21:36.590Z | 113.357° SE | 2026-03-25 16:23:36.590Z | 56.263° ENE | 25.582° | 2026-03-25 16:25:36.590Z | 16.584° NNE |
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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