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 00046U 60007B 25137.71567898 .00001357 00000-0 26596-3 0 9999
2 00046 66.6887 225.6010 0203180 231.7993 126.4671 14.53950929399495
| Epoch (UTC): | 17 May 2025 17:10:34 |
| Eccentricity: | 0.0203180 |
| inclination: | 66.6887° |
| perigee height: | 569 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 225.6010° |
| argument of perigee: | 231.7993° |
| revolutions per day: | 14.53950929 |
| mean anomaly at epoch: | 126.4671° |
| orbit number at epoch: | 39949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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