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 23079.13504639 .00000316 00000-0 14974-3 0 9991
2 25338 98.6167 109.6734 0009910 208.0668 151.9979 14.26271131292562
| Epoch (UTC): | 20 March 2023 03:14:28 |
| Eccentricity: | 0.0009910 |
| inclination: | 98.6167° |
| perigee height: | 797 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 109.6734° |
| argument of perigee: | 208.0668° |
| revolutions per day: | 14.26271131 |
| mean anomaly at epoch: | 151.9979° |
| orbit number at epoch: | 29256 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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