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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Edit Public Description
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: 4 hours ago
TLE from 4 hours ago
0 HORACIO
1 59098U 24043A 26040.52286392 .00003727 00000-0 32155-3 0 9991
2 59098 97.8319 171.6932 0012467 87.3536 272.9113 14.97843085105551Epoch: 2026-02-09T12:32Z
TLE epoch observation values (Epoch: 2026-02-09T12:32:55.442Z)
Latitude
-0.00001°
Longitude
-156.15427°
Altitude
576.18 km
Speed
7.573 km/s
True Right ascension
11h 26m 46s
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
19:18:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.239 km
Perigee altitude
561.913 km
Semi-major axis
6,948.713 km
Eccentricity
0.00125
Inclination
97.8319°
RAAN
171.6932°
Arg. of periapsis
87.3536°
True anomaly
272.76861°
Mean anomaly
272.9113°
Eccentric anomaly
272.83996°
Mean motion
3.74703 °/min
Orbital period
96.08 mins
BSTAR
0.00032155
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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 | 2026-02-09 21:08:17.343Z | 29.838° NE | 2026-02-09 21:11:17.343Z | 95.885° ESE | 35.237° | 2026-02-09 21:14:17.343Z | 167.784° S |
| 4 mins | 2026-02-10 07:57:17.343Z | 102.758° ESE | 2026-02-10 07:58:17.343Z | 80.123° E | 23.914° | 2026-02-10 08:01:17.343Z | 19.249° NNE |
| 4 mins | 2026-02-10 09:32:17.343Z | 234.067° WSW | 2026-02-10 09:34:17.343Z | 275.304° WNW | 19.821° | 2026-02-10 09:36:17.343Z | 309.241° NW |
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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