ACS 3, 59588
Orbit data source: Space-Track
ACS 3, 59588 is a payload satellite owned by ARC (US) in SSO that was launched on Tue, 23 Apr 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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59588 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ARC/NANAVU
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
16.1 kg wet, 16.1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Sail, 6.3 m
Radar Cross Section
0.080 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ACS 3
1 59588U 24077B 25322.32979231 .00048723 00000-0 42912-1 0 9998
2 59588 97.3002 283.3644 0064442 20.5237 339.8491 13.83990772 78761Epoch: 2025-11-18T07:54Z
TLE epoch observation values (Epoch: 2025-11-18T07:54:54.055Z)
Latitude
-0.00002°
Longitude
107.02174°
Altitude
908.368 km
Speed
7.42 km/s
True Right ascension
18h 53m 27s
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
13:58:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
994.116 km
Perigee altitude
899.708 km
Semi-major axis
7,325.049 km
Eccentricity
0.00644
Inclination
97.3002°
RAAN
283.3644°
Arg. of periapsis
20.5237°
True anomaly
339.59277°
Mean anomaly
339.8491°
Eccentric anomaly
339.72113°
Mean motion
3.462 °/min
Orbital period
103.99 mins
BSTAR
0.042912
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Other satellites on launch #77 in the year 2024 (2024-04-23 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.ACS 3 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-18 20:12:53.648Z | 105.291° ESE | 2025-11-18 20:16:53.648Z | 59.616° ENE | 18.123° | 2025-11-18 20:19:53.648Z | 25.489° NE |
| 9 mins | 2025-11-18 21:54:53.648Z | 184.895° SSW | 2025-11-18 21:58:53.648Z | 255.9° W | 41.094° | 2025-11-18 22:03:53.648Z | 339.146° N |
| 5 mins | 2025-11-19 08:50:53.648Z | 65.987° ENE | 2025-11-19 08:52:53.648Z | 87.477° E | 14.608° | 2025-11-19 08:55:53.648Z | 118.325° SE |
| 10 mins | 2025-11-19 10:31:53.648Z | 7.099° NNE | 2025-11-19 10:36:53.648Z | 240.646° WSW | 43.589° | 2025-11-19 10:41:53.648Z | 200.005° 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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