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 23087.97428211 .00000354 00000-0 16561-3 0 9999
2 25338 98.6156 118.3705 0010450 181.7253 178.3893 14.26278437293827
| Epoch (UTC): | 28 March 2023 23:22:57 |
| Eccentricity: | 0.0010450 |
| inclination: | 98.6156° |
| perigee height: | 796 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 118.3705° |
| argument of perigee: | 181.7253° |
| revolutions per day: | 14.26278437 |
| mean anomaly at epoch: | 178.3893° |
| orbit number at epoch: | 29382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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