HORACIO, 59098
Orbit data source: Space-Track
HORACIO, 59098 is a payload satellite owned by Satlantis (ES) in SSO that was launched on Mon, 04 Mar 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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59098 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U M16P, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 HORACIO
1 59098U 24043A 26235.58957216 .00002833 00000-0 23998-3 0 9995
2 59098 97.8606 7.8412 0012074 144.8197 215.3824 14.98767529134763Epoch: 2026-08-23T14:08Z
TLE epoch observation values (Epoch: 2026-08-23T14:08:59.034Z)
Latitude
-0.00011°
Longitude
-176.28821°
Altitude
580.597 km
Speed
7.566 km/s
True Right ascension
00h 31m 21s
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
15:54:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.104 km
Perigee altitude
559.331 km
Semi-major axis
6,945.854 km
Eccentricity
0.00121
Inclination
97.8606°
RAAN
7.8412°
Arg. of periapsis
144.8197°
True anomaly
215.30239°
Mean anomaly
215.3824°
Eccentric anomaly
215.34238°
Mean motion
3.74934 °/min
Orbital period
96.02 mins
BSTAR
0.00023998
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.HORACIO 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-24 07:56:19.705Z | 100.145° ESE | 2026-08-24 07:58:19.705Z | 64.836° ENE | 17.537° | 2026-08-24 08:00:19.705Z | 30.97° NE |
| 5 mins | 2026-08-24 09:31:19.705Z | 217.332° SW | 2026-08-24 09:33:19.705Z | 270.331° WNW | 28.381° | 2026-08-24 09:36:19.705Z | 324.652° NNW |
| 5 mins | 2026-08-24 21:11:19.705Z | 52.335° ENE | 2026-08-24 21:13:19.705Z | 101.474° ESE | 26.786° | 2026-08-24 21:16:19.705Z | 156.903° SSE |
| 4 mins | 2026-08-24 22:46:19.705Z | 324.913° NNW | 2026-08-24 22:48:19.705Z | 287.617° WNW | 18.135° | 2026-08-24 22:50:19.705Z | 253.58° W |
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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