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 60235U 24128A 24280.46412377 .00010043 00000-0 90329-3 0 9997
2 60235 61.9966 216.1217 0021942 325.7321 34.2349 14.95966245 13253
| Epoch (UTC): | 06 October 2024 11:08:20 |
| Eccentricity: | 0.0021942 |
| inclination: | 61.9966° |
| perigee height: | 564 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 216.1217° |
| argument of perigee: | 325.7321° |
| revolutions per day: | 14.95966245 |
| mean anomaly at epoch: | 34.2349° |
| orbit number at epoch: | 1325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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