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 12586U 81065B 24259.51221325 .00012978 00000-0 56646-3 0 9992
2 12586 97.6925 275.2429 0017118 102.2448 258.0706 15.22144401356626
| Epoch (UTC): | 15 September 2024 12:17:35 |
| Eccentricity: | 0.0017118 |
| inclination: | 97.6925° |
| perigee height: | 487 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 275.2429° |
| argument of perigee: | 102.2448° |
| revolutions per day: | 15.22144401 |
| mean anomaly at epoch: | 258.0706° |
| orbit number at epoch: | 35662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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