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: 7 hours ago
TLE from 7 hours ago
0 TOMORROW-S1
1 60479U 24149M 26080.48696678 .00010611 00000-0 35232-3 0 9993
2 60479 97.3780 161.3107 0002968 167.2007 192.9311 15.31398538 88669Epoch: 2026-03-21T11:41Z
TLE epoch observation values (Epoch: 2026-03-21T11:41:13.929Z)
Latitude
0.00003°
Longitude
166.99568°
Altitude
476.727 km
Speed
7.626 km/s
True Right ascension
10h 45m 14s
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
23:12:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.62 km
Perigee altitude
466.556 km
Semi-major axis
6,846.725 km
Eccentricity
0.0003
Inclination
97.378°
RAAN
161.3107°
Arg. of periapsis
167.2007°
True anomaly
192.92349°
Mean anomaly
192.9311°
Eccentric anomaly
192.9273°
Mean motion
3.83106 °/min
Orbital period
93.97 mins
BSTAR
0.00035232
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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 | 2026-03-21 18:31:01.549Z | 356.832° N | 2026-03-21 18:34:01.549Z | 274.679° WNW | 35.673° | 2026-03-21 18:37:01.549Z | 212.206° SW |
| 5 mins | 2026-03-22 05:05:01.549Z | 140.361° SSE | 2026-03-22 05:07:01.549Z | 71.027° E | 36.953° | 2026-03-22 05:10:01.549Z | 0.939° NNE |
| 4 mins | 2026-03-22 18:04:01.549Z | 26.975° NE | 2026-03-22 18:06:01.549Z | 148.637° SSE | 39.955° | 2026-03-22 18:08:01.549Z | 181.372° SSW |
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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