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 25137.91244814 .00000609 00000-0 17746-3 0 9996
2 00045 66.6941 325.3803 0242353 87.6088 275.2735 14.35532105323304
| Epoch (UTC): | 17 May 2025 21:53:55 |
| Eccentricity: | 0.0242353 |
| inclination: | 66.6941° |
| perigee height: | 600 km |
| apogee height: | 946 km |
| right ascension of ascending node: | 325.3803° |
| argument of perigee: | 87.6088° |
| revolutions per day: | 14.35532105 |
| mean anomaly at epoch: | 275.2735° |
| orbit number at epoch: | 32330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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