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 25109.92437397 .00001325 00000-0 25991-3 0 9994
2 00046 66.6881 301.2580 0204624 251.9650 105.9071 14.53850170395455
| Epoch (UTC): | 19 April 2025 22:11:05 |
| Eccentricity: | 0.0204624 |
| inclination: | 66.6881° |
| perigee height: | 568 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 301.2580° |
| argument of perigee: | 251.9650° |
| revolutions per day: | 14.53850170 |
| mean anomaly at epoch: | 105.9071° |
| orbit number at epoch: | 39545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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