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 00045U 60007A 23088.79452976 .00000700 00000-0 19667-3 0 9991
2 00045 66.6939 224.7091 0260846 295.7941 61.6456 14.34148081211396
| Epoch (UTC): | 29 March 2023 19:04:07 |
| Eccentricity: | 0.0260846 |
| inclination: | 66.6939° |
| perigee height: | 591 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 224.7091° |
| argument of perigee: | 295.7941° |
| revolutions per day: | 14.34148081 |
| mean anomaly at epoch: | 61.6456° |
| orbit number at epoch: | 21139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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