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 24262.27245832 .00000612 00000-0 82031-3 0 9997
2 00016 34.2788 347.0033 2025531 310.8904 33.2738 10.49419178621991
| Epoch (UTC): | 18 September 2024 06:32:20 |
| Eccentricity: | 0.2025531 |
| inclination: | 34.2788° |
| perigee height: | 649 km |
| apogee height: | 4219 km |
| right ascension of ascending node: | 347.0033° |
| argument of perigee: | 310.8904° |
| revolutions per day: | 10.49419178 |
| mean anomaly at epoch: | 33.2738° |
| orbit number at epoch: | 62199 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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