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 25338U 98030A 23333.77412681 .00000409 00000-0 18786-3 0 9997
2 25338 98.5904 359.8889 0010228 184.6598 175.4489 14.26444111328865
| Epoch (UTC): | 29 November 2023 18:34:44 |
| Eccentricity: | 0.0010228 |
| inclination: | 98.5904° |
| perigee height: | 796 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 359.8889° |
| argument of perigee: | 184.6598° |
| revolutions per day: | 14.26444111 |
| mean anomaly at epoch: | 175.4489° |
| orbit number at epoch: | 32886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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