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 23545U 95017A 23082.92372456 .00010942 00000-0 16450-2 0 9998
2 23545 69.9681 280.5552 0003557 144.6579 215.4804 14.74675220491650
| Epoch (UTC): | 23 March 2023 22:10:09 |
| Eccentricity: | 0.0003557 |
| inclination: | 69.9681° |
| perigee height: | 643 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 280.5552° |
| argument of perigee: | 144.6579° |
| revolutions per day: | 14.74675220 |
| mean anomaly at epoch: | 215.4804° |
| orbit number at epoch: | 49165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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