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 28095U 03054A 25149.88883033 0.00000270 00000-0 18067-3 0 05
2 28095 63.3858 78.3813 0571672 5.0507 354.9493 13.41927865 07
| Epoch (UTC): | 29 May 2025 21:19:54 |
| Eccentricity: | 0.0571672 |
| inclination: | 63.3858° |
| perigee height: | 674 km |
| apogee height: | 1530 km |
| right ascension of ascending node: | 78.3813° |
| argument of perigee: | 5.0507° |
| revolutions per day: | 13.41927865 |
| mean anomaly at epoch: | 354.9493° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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