MAKERSAT 0, 43016
Orbit data source: Space-Track
MAKERSAT 0, 43016 is a payload satellite owned by NW Nazarene (US) in SSO that was launched on Sat, 18 Nov 2017 UTC via a DELTA 7920-10C 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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43016 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NW Nazarene
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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 MAKERSAT 0
1 43016U 17073D 26187.63911722 .00016571 00000-0 44083-3 0 9999
2 43016 97.4596 70.3150 0104976 202.8118 156.8443 15.32782580469440Epoch: 2026-07-06T15:20Z
TLE epoch observation values (Epoch: 2026-07-06T15:20:19.727Z)
Latitude
-0.00007°
Longitude
-84.3884°
Altitude
536.824 km
Speed
7.557 km/s
True Right ascension
04h 41m 15s
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
21:46:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
536.296 km
Perigee altitude
392.634 km
Semi-major axis
6,842.602 km
Eccentricity
0.0105
Inclination
97.4596°
RAAN
70.315°
Arg. of periapsis
202.8118°
True anomaly
157.31169°
Mean anomaly
156.8443°
Eccentric anomaly
157.07855°
Mean motion
3.83452 °/min
Orbital period
93.88 mins
BSTAR
0.00044083
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Other satellites on launch #73 in the year 2017 (2017-11-18 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.MAKERSAT 0 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 | 2026-07-07 16:32:34.992Z | 188.723° SSW | 2026-07-07 16:34:34.992Z | 233.694° WSW | 37.741° | 2026-07-07 16:38:34.992Z | 337.73° N |
| 4 mins | 2026-07-08 05:31:34.992Z | 336.487° NNW | 2026-07-08 05:32:34.992Z | 305.581° NW | 29.935° | 2026-07-08 05:35:34.992Z | 220.924° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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