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 2802U 67045B 25194.39122623 .00000197 00000-0 62455-4 0 9996
2 2802 74.0113 74.9087 0063928 140.7445 219.8374 14.45387656 54549
| Epoch (UTC): | 13 July 2025 09:23:21 |
| Eccentricity: | 0.0063928 |
| inclination: | 74.0113° |
| perigee height: | 695 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 74.9087° |
| argument of perigee: | 140.7445° |
| revolutions per day: | 14.45387656 |
| mean anomaly at epoch: | 219.8374° |
| orbit number at epoch: | 5454 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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