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 25258U 98016A 23088.57761715 .00000036 00000-0 00000+0 0 9994
2 25258 9.7409 28.7195 0000765 317.0740 277.6568 1.00382121 91789
| Epoch (UTC): | 29 March 2023 13:51:46 |
| Eccentricity: | 0.0000765 |
| inclination: | 9.7409° |
| perigee height: | 35752 km |
| apogee height: | 35758 km |
| right ascension of ascending node: | 28.7195° |
| argument of perigee: | 317.0740° |
| revolutions per day: | 1.00382121 |
| mean anomaly at epoch: | 277.6568° |
| orbit number at epoch: | 9178 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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