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 02802U 67045B 25193.62987329 .00000188 00000-0 59778-4 0 9997
2 02802 74.0113 76.3301 0063948 142.3708 218.1951 14.45387264 54331
| Epoch (UTC): | 12 July 2025 15:07:01 |
| Eccentricity: | 0.0063948 |
| inclination: | 74.0113° |
| perigee height: | 695 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 76.3301° |
| argument of perigee: | 142.3708° |
| revolutions per day: | 14.45387264 |
| mean anomaly at epoch: | 218.1951° |
| orbit number at epoch: | 5433 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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