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 25189.85570449 .00000363 00000-0 87851-4 0 9995
2 00046 66.6887 83.6499 0198848 193.4598 166.1166 14.54022541407072
| Epoch (UTC): | 08 July 2025 20:32:12 |
| Eccentricity: | 0.0198848 |
| inclination: | 66.6887° |
| perigee height: | 571 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 83.6499° |
| argument of perigee: | 193.4598° |
| revolutions per day: | 14.54022541 |
| mean anomaly at epoch: | 166.1166° |
| orbit number at epoch: | 40707 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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