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 24287.88315374 .00005701 00000-0 51851-3 0 9991
2 60235 61.9964 190.5236 0022798 329.8775 30.1000 14.96116724 14367
| Epoch (UTC): | 13 October 2024 21:11:44 |
| Eccentricity: | 0.0022798 |
| inclination: | 61.9964° |
| perigee height: | 563 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 190.5236° |
| argument of perigee: | 329.8775° |
| revolutions per day: | 14.96116724 |
| mean anomaly at epoch: | 30.1000° |
| orbit number at epoch: | 1436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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