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: 8 hours ago
TLE from 8 hours ago
0 TOMORROW-S7
1 63631U 25081B 26104.96250956 .00000815 00000-0 84012-4 0 9993
2 63631 45.3940 304.0818 0002540 280.0023 80.0569 14.99404252 53686Epoch: 2026-04-14T23:06Z
TLE epoch observation values (Epoch: 2026-04-14T23:06:00.825Z)
Latitude
0°
Longitude
114.44713°
Altitude
568.474 km
Speed
7.579 km/s
True Right ascension
20h 16m 19s
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
13:28:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.025 km
Perigee altitude
568.495 km
Semi-major axis
6,948.397 km
Eccentricity
0.00025
Inclination
45.394°
RAAN
304.0818°
Arg. of periapsis
280.0023°
True anomaly
80.08557°
Mean anomaly
80.0569°
Eccentric anomaly
80.07124°
Mean motion
3.74728 °/min
Orbital period
96.07 mins
BSTAR
0.000084012
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-15 15:15:07.325Z | 178.271° S | 2026-04-15 15:18:07.325Z | 131.982° SE | 16.606° | 2026-04-15 15:20:07.325Z | 101.426° ESE |
| 7 mins | 2026-04-15 16:55:07.325Z | 238.744° WSW | 2026-04-15 16:58:07.325Z | 128.441° SE | 44.552° | 2026-04-15 17:02:07.325Z | 66.908° ENE |
| 6 mins | 2026-04-15 18:36:07.325Z | 286.755° WNW | 2026-04-15 18:39:07.325Z | 358.142° N | 33.824° | 2026-04-15 18:42:07.325Z | 58.71° ENE |
| 7 mins | 2026-04-15 20:17:07.325Z | 302.615° NW | 2026-04-15 20:20:07.325Z | 7.852° NNE | 35.151° | 2026-04-15 20:24:07.325Z | 83.882° E |
| 7 mins | 2026-04-15 21:58:07.325Z | 288.505° WNW | 2026-04-15 22:01:07.325Z | 201.045° SSW | 42.929° | 2026-04-15 22:05:07.325Z | 126.322° SE |
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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