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 28591U 74015C 23341.57878473 .00000279 00000-0 14735-3 0 9995
2 28591 99.0394 217.1548 0045805 242.6611 177.2298 14.21452319978724
| Epoch (UTC): | 07 December 2023 13:53:27 |
| Eccentricity: | 0.0045805 |
| inclination: | 99.0394° |
| perigee height: | 787 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 217.1548° |
| argument of perigee: | 242.6611° |
| revolutions per day: | 14.21452319 |
| mean anomaly at epoch: | 177.2298° |
| orbit number at epoch: | 97872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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