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 23343.10330541 .00000162 00000-0 85348-4 0 9994
2 25338 98.5897 9.0407 0010765 157.8547 202.3101 14.26450166330195
| Epoch (UTC): | 09 December 2023 02:28:45 |
| Eccentricity: | 0.0010765 |
| inclination: | 98.5897° |
| perigee height: | 796 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 9.0407° |
| argument of perigee: | 157.8547° |
| revolutions per day: | 14.26450166 |
| mean anomaly at epoch: | 202.3101° |
| orbit number at epoch: | 33019 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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