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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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: 1 day ago
TLE from 1 day ago
0 TOMORROW-S1
1 60479U 24149M 25301.19906030 .00009026 00000-0 33060-3 0 9997
2 60479 97.3967 17.8441 0002896 24.7056 335.4322 15.28240364 66608Epoch: 2025-10-28T04:46Z
TLE epoch observation values (Epoch: 2025-10-28T04:46:38.809Z)
Latitude
-0.00003°
Longitude
-90.60758°
Altitude
482.367 km
Speed
7.625 km/s
True Right ascension
01h 11m 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
08:14:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.012 km
Perigee altitude
476.041 km
Semi-major axis
6,856.164 km
Eccentricity
0.00029
Inclination
97.3967°
RAAN
17.8441°
Arg. of periapsis
24.7056°
True anomaly
335.4184°
Mean anomaly
335.4322°
Eccentric anomaly
335.4253°
Mean motion
3.82315 °/min
Orbital period
94.16 mins
BSTAR
0.0003306
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-29 17:29:57.559Z | 47.378° ENE | 2025-10-29 17:31:57.559Z | 93.017° ESE | 24.148° | 2025-10-29 17:34:57.559Z | 154.503° SSE |
| 6 mins | 2025-10-30 05:36:57.559Z | 188.986° SSW | 2025-10-30 05:39:57.559Z | 268.2° W | 35.474° | 2025-10-30 05:42:57.559Z | 333.977° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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