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 60672U 24140BZ 24357.45092445 .00015153 00000-0 20037-2 0 9995
2 60672 88.7451 329.6768 0164451 285.1713 73.1369 14.70829268 19865
| Epoch (UTC): | 22 December 2024 10:49:19 |
| Eccentricity: | 0.0164451 |
| inclination: | 88.7451° |
| perigee height: | 543 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 329.6768° |
| argument of perigee: | 285.1713° |
| revolutions per day: | 14.70829268 |
| mean anomaly at epoch: | 73.1369° |
| orbit number at epoch: | 1986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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