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 26906U 01040B 25136.30689537 .00000354 00000-0 26078-3 0 9994
2 26906 63.4246 102.8815 0594996 340.7390 17.1969 13.44951099 50028
| Epoch (UTC): | 16 May 2025 07:21:55 |
| Eccentricity: | 0.0594996 |
| inclination: | 63.4246° |
| perigee height: | 646 km |
| apogee height: | 1535 km |
| right ascension of ascending node: | 102.8815° |
| argument of perigee: | 340.7390° |
| revolutions per day: | 13.44951099 |
| mean anomaly at epoch: | 17.1969° |
| orbit number at epoch: | 5002 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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