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, 1.0 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 HORACIO
1 59098U 24043A 26187.31722573 .00002836 00000-0 24138-3 0 9998
2 59098 97.8544 319.2182 0008902 325.2466 34.8174 14.98607135127532Epoch: 2026-07-06T07:36Z
TLE epoch observation values (Epoch: 2026-07-06T07:36:48.303Z)
Latitude
0.00003°
Longitude
-79.28701°
Altitude
569.169 km
Speed
7.579 km/s
True Right ascension
21h 16m 52s
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
01:37:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.397 km
Perigee altitude
562.029 km
Semi-major axis
6,946.35 km
Eccentricity
0.00089
Inclination
97.8544°
RAAN
319.2182°
Arg. of periapsis
325.2466°
True anomaly
34.8757°
Mean anomaly
34.8174°
Eccentric anomaly
34.84654°
Mean motion
3.74894 °/min
Orbital period
96.03 mins
BSTAR
0.00024138
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-06 21:00:56.715Z | 44.495° NE | 2026-07-06 21:03:56.715Z | 104.329° ESE | 24.296° | 2026-07-06 21:06:56.715Z | 153.927° SSE |
| 4 mins | 2026-07-06 22:36:56.715Z | 325.001° NNW | 2026-07-06 22:38:56.715Z | 284.357° WNW | 20.644° | 2026-07-06 22:40:56.715Z | 249.14° W |
| 6 mins | 2026-07-07 09:22:56.715Z | 202.173° SSW | 2026-07-07 09:25:56.715Z | 273.4° WNW | 30.053° | 2026-07-07 09:28:56.715Z | 327.047° 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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