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 23340.78855026 .00000224 00000-0 11118-3 0 9997
2 25338 98.5900 6.7701 0010634 164.3326 195.8186 14.26449094329863
| Epoch (UTC): | 06 December 2023 18:55:30 |
| Eccentricity: | 0.0010634 |
| inclination: | 98.5900° |
| perigee height: | 796 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 6.7701° |
| argument of perigee: | 164.3326° |
| revolutions per day: | 14.26449094 |
| mean anomaly at epoch: | 195.8186° |
| orbit number at epoch: | 32986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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