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 23335.45759109 .00000406 00000-0 18665-3 0 9996
2 25338 98.5903 1.5405 0010355 179.6403 180.4787 14.26445666329100
| Epoch (UTC): | 01 December 2023 10:58:55 |
| Eccentricity: | 0.0010355 |
| inclination: | 98.5903° |
| perigee height: | 796 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 1.5405° |
| argument of perigee: | 179.6403° |
| revolutions per day: | 14.26445666 |
| mean anomaly at epoch: | 180.4787° |
| orbit number at epoch: | 32910 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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