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 23342.12128824 .00000164 00000-0 86193-4 0 9995
2 25338 98.5898 8.0774 0010711 160.6155 199.5435 14.26449690330052
| Epoch (UTC): | 08 December 2023 02:54:39 |
| Eccentricity: | 0.0010711 |
| inclination: | 98.5898° |
| perigee height: | 796 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 8.0774° |
| argument of perigee: | 160.6155° |
| revolutions per day: | 14.26449690 |
| mean anomaly at epoch: | 199.5435° |
| orbit number at epoch: | 33005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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