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: 8 hours ago
TLE from 8 hours ago
0 HORACIO
1 59098U 24043A 26042.59378031 .00003042 00000-0 26332-3 0 9992
2 59098 97.8316 173.7706 0012286 80.9045 279.3566 14.97856170105869Epoch: 2026-02-11T14:15Z
TLE epoch observation values (Epoch: 2026-02-11T14:15:02.618Z)
Latitude
-0.00009°
Longitude
178.35205°
Altitude
575.191 km
Speed
7.574 km/s
True Right ascension
11h 35m 04s
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
00:51:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.073 km
Perigee altitude
561.998 km
Semi-major axis
6,948.673 km
Eccentricity
0.00123
Inclination
97.8316°
RAAN
173.7706°
Arg. of periapsis
80.9045°
True anomaly
279.21765°
Mean anomaly
279.3566°
Eccentric anomaly
279.28713°
Mean motion
3.74706 °/min
Orbital period
96.08 mins
BSTAR
0.00026332
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-12 08:02:06.691Z | 122.552° SE | 2026-02-12 08:04:06.691Z | 82.231° E | 26.736° | 2026-02-12 08:07:06.691Z | 16.366° NNE |
| 4 mins | 2026-02-12 09:38:06.691Z | 236.572° WSW | 2026-02-12 09:40:06.691Z | 273.946° WNW | 17.49° | 2026-02-12 09:42:06.691Z | 306.354° NW |
| 6 mins | 2026-02-12 21:18:06.691Z | 30.762° NE | 2026-02-12 21:20:06.691Z | 97.684° ESE | 40.311° | 2026-02-12 21:24:06.691Z | 180.57° 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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