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: 8 hours ago
TLE from 8 hours ago
0 ACS 3
1 59588U 24077B 25352.89174389 .00016414 00000-0 14003-1 0 9996
2 59588 97.2636 307.1233 0076429 323.2471 36.3464 13.85760768 82994Epoch: 2025-12-18T21:24Z
TLE epoch observation values (Epoch: 2025-12-18T21:24:06.672Z)
Latitude
0.00001°
Longitude
-101.64524°
Altitude
901.505 km
Speed
7.424 km/s
True Right ascension
20h 28m 29s
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
04:24:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
996.603 km
Perigee altitude
884.73 km
Semi-major axis
7,318.804 km
Eccentricity
0.00764
Inclination
97.2636°
RAAN
307.1233°
Arg. of periapsis
323.2471°
True anomaly
36.86948°
Mean anomaly
36.3464°
Eccentric anomaly
36.60754°
Mean motion
3.46643 °/min
Orbital period
103.85 mins
BSTAR
0.014003
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-19 08:25:58.064Z | 57.698° ENE | 2025-12-19 08:28:58.064Z | 88.819° E | 15.36° | 2025-12-19 08:31:58.064Z | 119.515° SE |
| 10 mins | 2025-12-19 10:07:58.064Z | 6.183° NNE | 2025-12-19 10:11:58.064Z | 309.88° NW | 43.933° | 2025-12-19 10:17:58.064Z | 200.427° SSW |
| 8 mins | 2025-12-19 20:04:58.064Z | 111.979° ESE | 2025-12-19 20:07:58.064Z | 73.197° E | 24.411° | 2025-12-19 20:12:58.064Z | 12.925° NNE |
| 9 mins | 2025-12-19 21:46:58.064Z | 200.391° SSW | 2025-12-19 21:50:58.064Z | 266.069° W | 34.45° | 2025-12-19 21:55:58.064Z | 332.703° NNW |
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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