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: 8 hours ago
TLE from 8 hours ago
0 TOMORROW-S1
1 60479U 24149M 26260.21925130 .00006492 00000-0 20065-3 0 9992
2 60479 97.3686 340.4461 0000898 278.8705 81.2436 15.33861448116196Epoch: 2026-09-17T05:15Z
TLE epoch observation values (Epoch: 2026-09-17T05:15:43.312Z)
Latitude
-0.00002°
Longitude
-94.644°
Altitude
467.321 km
Speed
7.633 km/s
True Right ascension
22h 41m 47s
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
06:20:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.864 km
Perigee altitude
460.636 km
Semi-major axis
6,839.387 km
Eccentricity
0.00009
Inclination
97.3686°
RAAN
340.4461°
Arg. of periapsis
278.8705°
True anomaly
81.25377°
Mean anomaly
81.2436°
Eccentric anomaly
81.24869°
Mean motion
3.83723 °/min
Orbital period
93.82 mins
BSTAR
0.00020065
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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 | 2026-09-17 18:21:07.980Z | 10.735° NNE | 2026-09-17 18:24:07.980Z | 200.951° SSW | 65.772° | 2026-09-17 18:27:07.980Z | 194.191° SSW |
| 4 mins | 2026-09-18 04:54:07.980Z | 114.417° SE | 2026-09-18 04:56:07.980Z | 61.029° ENE | 26.363° | 2026-09-18 04:58:07.980Z | 19.198° 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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