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 60209U 24125G 25018.83413660 .00023347 00000-0 83215-3 0 9999
2 60209 97.2951 232.5778 0020830 286.8350 73.0605 15.28706147 30242
| Epoch (UTC): | 18 January 2025 20:01:09 |
| Eccentricity: | 0.0020830 |
| inclination: | 97.2951° |
| perigee height: | 465 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 232.5778° |
| argument of perigee: | 286.8350° |
| revolutions per day: | 15.28706147 |
| mean anomaly at epoch: | 73.0605° |
| orbit number at epoch: | 3024 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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