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 24285.47706567 .00015536 00000-0 13822-2 0 9994
2 60235 61.9960 198.8261 0022503 328.5739 31.4002 14.96085157 14004
| Epoch (UTC): | 11 October 2024 11:26:58 |
| Eccentricity: | 0.0022503 |
| inclination: | 61.9960° |
| perigee height: | 563 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 198.8261° |
| argument of perigee: | 328.5739° |
| revolutions per day: | 14.96085157 |
| mean anomaly at epoch: | 31.4002° |
| orbit number at epoch: | 1400 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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