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 12544U 81057A 23081.40535591 -.00000223 00000-0 00000+0 0 9990
2 12544 12.2767 327.6815 0028878 355.6785 356.7179 0.98726553112206
| Epoch (UTC): | 22 March 2023 09:43:42 |
| Eccentricity: | 0.0028878 |
| inclination: | 12.2767° |
| perigee height: | 36102 km |
| apogee height: | 36348 km |
| right ascension of ascending node: | 327.6815° |
| argument of perigee: | 355.6785° |
| revolutions per day: | 0.98726553 |
| mean anomaly at epoch: | 356.7179° |
| orbit number at epoch: | 11220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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