AO-95, 43770
Orbit data source: Space-Track
AO-95, 43770 is a payload satellite owned by AMSAT-NA (US) in SSO that was launched on Mon, 03 Dec 2018 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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43770 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AMSAT-NA
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 AO-95
1 43770U 18099N 26079.14479613 .00009795 00000-0 39894-3 0 9993
2 43770 97.4480 139.8092 0007518 305.5915 54.4622 15.24665968399642Epoch: 2026-03-20T03:28Z
TLE epoch observation values (Epoch: 2026-03-20T03:28:30.385Z)
Latitude
0.00003°
Longitude
-90.00148°
Altitude
491.884 km
Speed
7.621 km/s
True Right ascension
09h 19m 14s
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
14:31:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.913 km
Perigee altitude
483.588 km
Semi-major axis
6,866.887 km
Eccentricity
0.00075
Inclination
97.448°
RAAN
139.8092°
Arg. of periapsis
305.5915°
True anomaly
54.53234°
Mean anomaly
54.4622°
Eccentric anomaly
54.49727°
Mean motion
3.8142 °/min
Orbital period
94.38 mins
BSTAR
0.00039894
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.AO-95 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 | 2026-03-21 16:16:35.648Z | 40.924° NE | 2026-03-21 16:19:35.648Z | 112.418° ESE | 25.467° | 2026-03-21 16:21:35.648Z | 152.593° SSE |
| 5 mins | 2026-03-22 04:26:35.648Z | 203.131° SW | 2026-03-22 04:28:35.648Z | 264.766° W | 32.764° | 2026-03-22 04:31:35.648Z | 330.526° 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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