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 60691U 24140CU 24357.88188460 .00002865 00000-0 77531-3 0 9994
2 60691 89.0470 335.6932 0082263 328.3937 31.2341 14.45540920 19580
| Epoch (UTC): | 22 December 2024 21:09:54 |
| Eccentricity: | 0.0082263 |
| inclination: | 89.0470° |
| perigee height: | 681 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 335.6932° |
| argument of perigee: | 328.3937° |
| revolutions per day: | 14.45540920 |
| mean anomaly at epoch: | 31.2341° |
| orbit number at epoch: | 1958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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