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 00045U 60007A 25338.82711725 .00000598 00000-0 16862-3 0 9994
2 00045 66.6918 154.2588 0255334 300.2388 57.3656 14.35771608352145
| Epoch (UTC): | 04 December 2025 19:51:02 |
| Eccentricity: | 0.0255334 |
| inclination: | 66.6918° |
| perigee height: | 590 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 154.2588° |
| argument of perigee: | 300.2388° |
| revolutions per day: | 14.35771608 |
| mean anomaly at epoch: | 57.3656° |
| orbit number at epoch: | 35214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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