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 26575U 00065A 23088.38556578 -.00000327 00000-0 00000-0 0 9997
2 26575 9.5848 43.9763 0001557 281.0709 134.8262 1.00273335 21146
| Epoch (UTC): | 29 March 2023 09:15:12 |
| Eccentricity: | 0.0001557 |
| inclination: | 9.5848° |
| perigee height: | 35779 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 43.9763° |
| argument of perigee: | 281.0709° |
| revolutions per day: | 1.00273335 |
| mean anomaly at epoch: | 134.8262° |
| orbit number at epoch: | 2114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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