View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 00016U 58002A 23091.38804217 .00000141 00000-0 17280-3 0 9997
2 00016 34.2683 95.0711 2025488 210.1762 136.5138 10.48821314565719
| Epoch (UTC): | 01 April 2023 09:18:46 |
| Eccentricity: | 0.2025488 |
| inclination: | 34.2683° |
| perigee height: | 652 km |
| apogee height: | 4223 km |
| right ascension of ascending node: | 95.0711° |
| argument of perigee: | 210.1762° |
| revolutions per day: | 10.48821314 |
| mean anomaly at epoch: | 136.5138° |
| orbit number at epoch: | 56571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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