TOMORROW-S7, 63631
Orbit data source: Space-Track
TOMORROW-S7, 63631 is a payload satellite owned by Tomorrow.io (US) in LEO that was launched on Tue, 22 Apr 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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63631 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: 10 hours ago
TLE from 10 hours ago
0 TOMORROW-S7
1 63631U 25081B 26306.46598880 .00000803 00000-0 81886-4 0 9996
2 63631 45.3926 337.5938 0003522 287.6027 72.4467 14.99997990 83931Epoch: 2026-11-02T11:11Z
TLE epoch observation values (Epoch: 2026-11-02T11:11:01.432Z)
Latitude
0.00002°
Longitude
128.09525°
Altitude
566.208 km
Speed
7.58 km/s
True Right ascension
22h 30m 22s
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
16:51:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.874 km
Perigee altitude
565.981 km
Semi-major axis
6,946.564 km
Eccentricity
0.00035
Inclination
45.3926°
RAAN
337.5938°
Arg. of periapsis
287.6027°
True anomaly
72.48519°
Mean anomaly
72.4467°
Eccentric anomaly
72.46594°
Mean motion
3.74876 °/min
Orbital period
96.03 mins
BSTAR
0.000081886
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Other satellites on launch #81 in the year 2025 (2025-04-22 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-S7 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-03 04:56:18.691Z | 209.727° SW | 2026-11-03 05:00:18.691Z | 136.688° SSE | 35.122° | 2026-11-03 05:03:18.691Z | 82.349° E |
| 6 mins | 2026-11-03 06:38:18.691Z | 267.407° W | 2026-11-03 06:40:18.691Z | 317.875° NNW | 59.765° | 2026-11-03 06:44:18.691Z | 61.104° ENE |
| 6 mins | 2026-11-03 08:19:18.691Z | 302.608° NW | 2026-11-03 08:21:18.691Z | 345.52° N | 37.407° | 2026-11-03 08:25:18.691Z | 67.234° ENE |
| 6 mins | 2026-11-03 10:00:18.691Z | 304.148° NW | 2026-11-03 10:03:18.691Z | 53.446° ENE | 56.477° | 2026-11-03 10:06:18.691Z | 98.149° ESE |
| 5 mins | 2026-11-03 11:41:18.691Z | 265.875° W | 2026-11-03 11:43:18.691Z | 217.145° SW | 35.79° | 2026-11-03 11:46:18.691Z | 155.583° SSE |
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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