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Currently, to launch a satellite into a specific orbit, we adjust the apoapsis, periapsis and then perform an inclination change. The inclination change does not change the magnitude of the velocity, …
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What should this feature enhancement do?
Let the user zoom to distances in the thousands of kilometers above Earth.
This feature would be very handy for showing the current position of highly
ec…
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It would be nice to see a graphic visualization of the orbital positions of objects in TruSat database around Earth. This module should include some form of 3D visualization of Earth and orbiting sate…
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🐞 **Problem**
poliastro supports equinoctial elements, but test coverage is low and some conversions are not implemented.
🎯 **Goal**
Improve equinoctial element handling and showcase its adva…
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The maxelevation-sat unit test takes an order of magnitude longer time for Molniya 1 and Sirius 1 than for any other satellite. Is there potential for some optimization? Or are we just computing more …
ryeng updated
6 years ago
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```
What steps will reproduce the problem?
1. Put a placemark or graphical icon at 36,000 km altitude (36000000 meters).
This is the
altitude of a geosynchronous satellite.
2. Zoom out as far as G…
-
```
What steps will reproduce the problem?
1. Put a placemark or graphical icon at 36,000 km altitude (36000000 meters).
This is the
altitude of a geosynchronous satellite.
2. Zoom out as far as G…
-
```
What steps will reproduce the problem?
1. Put a placemark or graphical icon at 36,000 km altitude (36000000 meters).
This is the
altitude of a geosynchronous satellite.
2. Zoom out as far as G…
-
```
What steps will reproduce the problem?
1. Put a placemark or graphical icon at 36,000 km altitude (36000000 meters).
This is the
altitude of a geosynchronous satellite.
2. Zoom out as far as G…
-
```
What should this feature enhancement do?
Let the user zoom to distances in the thousands of kilometers above Earth.
This feature would be very handy for showing the current position of highly
ec…