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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Edit Public Description
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 25288.65783510 .00006477 00000-0 30766-3 0 9991
2 63225 97.4221 180.3625 0003604 275.5325 84.5499 15.19560041 32671Epoch: 2025-10-15T15:47Z
TLE epoch observation values (Epoch: 2025-10-15T15:47:16.952Z)
Latitude
-0.00001°
Longitude
-80.88689°
Altitude
510.024 km
Speed
7.609 km/s
True Right ascension
12h 01m 27s
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
22:45:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.617 km
Perigee altitude
501.656 km
Semi-major axis
6,882.273 km
Eccentricity
0.00036
Inclination
97.4221°
RAAN
180.3625°
Arg. of periapsis
275.5325°
True anomaly
84.59101°
Mean anomaly
84.5499°
Eccentric anomaly
84.57046°
Mean motion
3.80142 °/min
Orbital period
94.7 mins
BSTAR
0.00030766
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-16 05:00:37.922Z | 48.612° ENE | 2025-10-16 05:02:37.922Z | 85.657° E | 20.334° | 2025-10-16 05:05:37.922Z | 144.557° SSE |
| 4 mins | 2025-10-16 06:35:37.922Z | 317.153° NNW | 2025-10-16 06:36:37.922Z | 294.49° NW | 20.392° | 2025-10-16 06:39:37.922Z | 239.4° WSW |
| 5 mins | 2025-10-16 17:12:37.922Z | 188.355° SSW | 2025-10-16 17:14:37.922Z | 240.398° WSW | 38.522° | 2025-10-16 17:17:37.922Z | 334.641° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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