TOMORROW-S1, 60479
Orbit data source: Space-Track
TOMORROW-S1, 60479 is a payload satellite owned by Tomorrow.io (US) in SSO that was launched on Fri, 16 Aug 2024 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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60479 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: 9 hours ago
TLE from 9 hours ago
0 TOMORROW-S1
1 60479U 24149M 26171.46590854 .00006061 00000-0 19407-3 0 9991
2 60479 97.3745 251.9280 0001876 197.8929 162.2248 15.32758998102596Epoch: 2026-06-20T11:10Z
TLE epoch observation values (Epoch: 2026-06-20T11:10:54.497Z)
Latitude
0.00002°
Longitude
175.52079°
Altitude
471.917 km
Speed
7.629 km/s
True Right ascension
16h 47m 42s
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
07:23:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.816 km
Perigee altitude
463.249 km
Semi-major axis
6,842.669 km
Eccentricity
0.00019
Inclination
97.3745°
RAAN
251.928°
Arg. of periapsis
197.8929°
True anomaly
162.23136°
Mean anomaly
162.2248°
Eccentric anomaly
162.22808°
Mean motion
3.83447 °/min
Orbital period
93.89 mins
BSTAR
0.00019407
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-S1 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 | 2026-06-21 04:34:16.513Z | 107.339° ESE | 2026-06-21 04:36:16.513Z | 68.63° E | 16.918° | 2026-06-21 04:38:16.513Z | 30.238° NE |
| 4 mins | 2026-06-21 17:32:16.513Z | 59.154° ENE | 2026-06-21 17:34:16.513Z | 106° ESE | 19.566° | 2026-06-21 17:36:16.513Z | 143.66° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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