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 24263.81877608 .00005511 00000-0 50758-3 0 9995
2 60235 61.9950 273.5365 0020253 315.1756 44.7695 14.95704335 10769
| Epoch (UTC): | 19 September 2024 19:39:02 |
| Eccentricity: | 0.0020253 |
| inclination: | 61.9950° |
| perigee height: | 566 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 273.5365° |
| argument of perigee: | 315.1756° |
| revolutions per day: | 14.95704335 |
| mean anomaly at epoch: | 44.7695° |
| orbit number at epoch: | 1076 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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