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 21799U 91076C 23075.84621631 0.00006200 00000-0 75376-3 0 01
2 21799 63.3152 57.7529 0899218 53.4399 306.5601 13.43738542 06
| Epoch (UTC): | 16 March 2023 20:18:33 |
| Eccentricity: | 0.0899218 |
| inclination: | 63.3152° |
| perigee height: | 423 km |
| apogee height: | 1767 km |
| right ascension of ascending node: | 57.7529° |
| argument of perigee: | 53.4399° |
| revolutions per day: | 13.43738542 |
| mean anomaly at epoch: | 306.5601° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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