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 00046U 60007B 23080.53460355 .00001796 00000-0 37805-3 0 9996
2 00046 66.6910 204.2019 0199912 100.4254 261.9451 14.50294521285078
| Epoch (UTC): | 21 March 2023 12:49:49 |
| Eccentricity: | 0.0199912 |
| inclination: | 66.6910° |
| perigee height: | 582 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 204.2019° |
| argument of perigee: | 100.4254° |
| revolutions per day: | 14.50294521 |
| mean anomaly at epoch: | 261.9451° |
| orbit number at epoch: | 28507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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