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 25343.09929909 .00036419 00000-0 74576-3 0 9990
2 60209 97.2524 193.4693 0013842 191.9977 168.0945 15.45905039 80040
| Epoch (UTC): | 09 December 2025 02:22:59 |
| Eccentricity: | 0.0013842 |
| inclination: | 97.2524° |
| perigee height: | 419 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 193.4693° |
| argument of perigee: | 191.9977° |
| revolutions per day: | 15.45905039 |
| mean anomaly at epoch: | 168.0945° |
| orbit number at epoch: | 8004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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