TOMORROW-S5, 63234
Orbit data source: Space-Track
TOMORROW-S5, 63234 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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63234 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: 11 hours ago
TLE from 11 hours ago
0 TOMORROW-S5
1 63234U 25052AA 26074.65138767 .00005598 00000-0 25111-3 0 9994
2 63234 97.4098 328.8038 0008416 113.6855 246.5265 15.21570468 55613Epoch: 2026-03-15T15:37Z
TLE epoch observation values (Epoch: 2026-03-15T15:37:59.894Z)
Latitude
-0.00003°
Longitude
-78.95091°
Altitude
506.506 km
Speed
7.61 km/s
True Right ascension
21h 55m 12s
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
07:25:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.854 km
Perigee altitude
492.28 km
Semi-major axis
6,876.204 km
Eccentricity
0.00084
Inclination
97.4098°
RAAN
328.8038°
Arg. of periapsis
113.6855°
True anomaly
246.43808°
Mean anomaly
246.5265°
Eccentric anomaly
246.48229°
Mean motion
3.80645 °/min
Orbital period
94.58 mins
BSTAR
0.00025111
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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-S5 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 | 2026-03-16 04:50:38.597Z | 56.875° ENE | 2026-03-16 04:52:38.597Z | 93.388° ESE | 16.277° | 2026-03-16 04:54:38.597Z | 130.212° SE |
| 4 mins | 2026-03-16 06:24:38.597Z | 332.407° NNW | 2026-03-16 06:26:38.597Z | 282.674° WNW | 24.24° | 2026-03-16 06:28:38.597Z | 239.345° WSW |
| 5 mins | 2026-03-16 17:01:38.597Z | 176.237° S | 2026-03-16 17:03:38.597Z | 247.853° W | 43.944° | 2026-03-16 17:06:38.597Z | 343.321° N |
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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