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 25757U 99029B 23088.85764490 .00000420 00000-0 11637-3 0 9996
2 25757 98.5254 39.7549 0013768 332.9247 27.1228 14.51624160262689
| Epoch (UTC): | 29 March 2023 20:35:00 |
| Eccentricity: | 0.0013768 |
| inclination: | 98.5254° |
| perigee height: | 710 km |
| apogee height: | 730 km |
| right ascension of ascending node: | 39.7549° |
| argument of perigee: | 332.9247° |
| revolutions per day: | 14.51624160 |
| mean anomaly at epoch: | 27.1228° |
| orbit number at epoch: | 26268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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