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 06080U 72049B 25189.57430203 .00000052 00000-0 26739-4 0 9993
2 06080 81.2381 42.7336 0048037 304.3750 55.2877 14.01244578709071
| Epoch (UTC): | 08 July 2025 13:46:59 |
| Eccentricity: | 0.0048037 |
| inclination: | 81.2381° |
| perigee height: | 854 km |
| apogee height: | 924 km |
| right ascension of ascending node: | 42.7336° |
| argument of perigee: | 304.3750° |
| revolutions per day: | 14.01244578 |
| mean anomaly at epoch: | 55.2877° |
| orbit number at epoch: | 70907 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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