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: 11 hours ago
TLE from 11 hours ago
0 TOMORROW-S1
1 60479U 24149M 26131.96159620 .00004502 00000-0 14729-3 0 9994
2 60479 97.3750 212.5631 0003278 48.6179 311.5344 15.32206006 96544Epoch: 2026-05-11T23:04Z
TLE epoch observation values (Epoch: 2026-05-11T23:04:41.911Z)
Latitude
-0.00006°
Longitude
-3.35433°
Altitude
470.852 km
Speed
7.631 km/s
True Right ascension
14h 10m 15s
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
18:12:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.424 km
Perigee altitude
463.937 km
Semi-major axis
6,844.317 km
Eccentricity
0.00033
Inclination
97.375°
RAAN
212.5631°
Arg. of periapsis
48.6179°
True anomaly
311.50627°
Mean anomaly
311.5344°
Eccentric anomaly
311.52034°
Mean motion
3.83308 °/min
Orbital period
93.92 mins
BSTAR
0.00014729
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-12 18:26:38.088Z | 1.767° NNE | 2026-05-12 18:29:38.088Z | 272.421° WNW | 40.09° | 2026-05-12 18:32:38.088Z | 206.132° SW |
| 4 mins | 2026-05-13 05:00:38.088Z | 127.923° SE | 2026-05-13 05:02:38.088Z | 58.339° ENE | 31.449° | 2026-05-13 05:04:38.088Z | 10.994° NNE |
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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