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 25191.41502678 .00000178 00000-0 57223-4 0 9994
2 02802 74.0115 80.4648 0064007 147.1031 213.4137 14.45386218 54019
| Epoch (UTC): | 10 July 2025 09:57:38 |
| Eccentricity: | 0.0064007 |
| inclination: | 74.0115° |
| perigee height: | 695 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 80.4648° |
| argument of perigee: | 147.1031° |
| revolutions per day: | 14.45386218 |
| mean anomaly at epoch: | 213.4137° |
| orbit number at epoch: | 5401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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