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 25138.74849288 .00000570 00000-0 16795-3 0 9994
2 00045 66.6941 323.1707 0242349 86.9793 275.9009 14.35532981323429
| Epoch (UTC): | 18 May 2025 17:57:49 |
| Eccentricity: | 0.0242349 |
| inclination: | 66.6941° |
| perigee height: | 600 km |
| apogee height: | 946 km |
| right ascension of ascending node: | 323.1707° |
| argument of perigee: | 86.9793° |
| revolutions per day: | 14.35532981 |
| mean anomaly at epoch: | 275.9009° |
| orbit number at epoch: | 32342 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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