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: 12 hours ago
TLE from 12 hours ago
0 TOMORROW-S6
1 63225U 25052R 26129.64739425 .00003177 00000-0 14177-3 0 9993
2 63225 97.4049 23.1420 0003345 271.1076 88.9777 15.22101700 63985Epoch: 2026-05-09T15:32Z
TLE epoch observation values (Epoch: 2026-05-09T15:32:14.863Z)
Latitude
-0.00001°
Longitude
-77.38175°
Altitude
502.555 km
Speed
7.613 km/s
True Right ascension
01h 32m 34s
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
11:57:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.765 km
Perigee altitude
494.166 km
Semi-major axis
6,874.602 km
Eccentricity
0.00033
Inclination
97.4049°
RAAN
23.142°
Arg. of periapsis
271.1076°
True anomaly
89.01603°
Mean anomaly
88.9777°
Eccentric anomaly
88.99686°
Mean motion
3.80778 °/min
Orbital period
94.54 mins
BSTAR
0.00014177
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-10 06:19:08.691Z | 329.029° NNW | 2026-05-10 06:20:08.691Z | 301.613° NW | 27.62° | 2026-05-10 06:23:08.691Z | 228.972° WSW |
| 5 mins | 2026-05-10 16:55:08.691Z | 166.09° S | 2026-05-10 16:57:08.691Z | 160.931° S | 43.59° | 2026-05-10 17:00:08.691Z | 348.67° N |
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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