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: 11 hours ago
TLE from 11 hours ago
0 TOMORROW-S6
1 63225U 25052R 25334.67690571 .00005397 00000-0 25177-3 0 9999
2 63225 97.4204 225.6295 0007101 103.6188 256.5839 15.20244546 39668Epoch: 2025-11-30T16:14Z
TLE epoch observation values (Epoch: 2025-11-30T16:14:44.653Z)
Latitude
0.00004°
Longitude
-87.84389°
Altitude
509.33 km
Speed
7.609 km/s
True Right ascension
15h 02m 31s
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
01:14:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.954 km
Perigee altitude
497.183 km
Semi-major axis
6,880.205 km
Eccentricity
0.00071
Inclination
97.4204°
RAAN
225.6295°
Arg. of periapsis
103.6188°
True anomaly
256.50477°
Mean anomaly
256.5839°
Eccentric anomaly
256.54433°
Mean motion
3.80313 °/min
Orbital period
94.66 mins
BSTAR
0.00025177
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.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 | 2025-12-01 05:27:09.571Z | 27.812° NE | 2025-12-01 05:30:09.571Z | 115.551° SE | 36.358° | 2025-12-01 05:33:09.571Z | 174.244° S |
| 5 mins | 2025-12-01 16:05:09.571Z | 116.092° SE | 2025-12-01 16:08:09.571Z | 60.668° ENE | 18.445° | 2025-12-01 16:10:09.571Z | 25.293° NE |
| 4 mins | 2025-12-01 17:40:09.571Z | 231.836° WSW | 2025-12-01 17:41:09.571Z | 255.29° W | 21.929° | 2025-12-01 17:44:09.571Z | 316.433° 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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