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 28372U 04025G 23274.49500110 .00000758 00000-0 20449-3 0 9993
2 28372 98.5584 245.9759 0044445 283.9106 75.7146 14.50282405 18419
| Epoch (UTC): | 01 October 2023 11:52:48 |
| Eccentricity: | 0.0044445 |
| inclination: | 98.5584° |
| perigee height: | 693 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 245.9759° |
| argument of perigee: | 283.9106° |
| revolutions per day: | 14.50282405 |
| mean anomaly at epoch: | 75.7146° |
| orbit number at epoch: | 1841 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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