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 26931U 01043C 25109.51057907 .00000414 00000-0 18611-3 0 9999
2 26931 67.0502 259.8760 0005588 270.9933 89.0528 14.31700662229958
| Epoch (UTC): | 19 April 2025 12:15:14 |
| Eccentricity: | 0.0005588 |
| inclination: | 67.0502° |
| perigee height: | 782 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 259.8760° |
| argument of perigee: | 270.9933° |
| revolutions per day: | 14.31700662 |
| mean anomaly at epoch: | 89.0528° |
| orbit number at epoch: | 22995 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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