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 24281.53358480 .00011603 00000-0 10400-2 0 9994
2 60235 61.9965 212.4321 0022072 326.2871 33.6812 14.95991050 13416
| Epoch (UTC): | 07 October 2024 12:48:21 |
| Eccentricity: | 0.0022072 |
| inclination: | 61.9965° |
| perigee height: | 564 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 212.4321° |
| argument of perigee: | 326.2871° |
| revolutions per day: | 14.95991050 |
| mean anomaly at epoch: | 33.6812° |
| orbit number at epoch: | 1341 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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