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 25118.73177961 .00000434 00000-0 19359-3 0 9998
2 26931 67.0509 236.0354 0005653 272.0234 88.0221 14.31711029231110
| Epoch (UTC): | 28 April 2025 17:33:45 |
| Eccentricity: | 0.0005653 |
| inclination: | 67.0509° |
| perigee height: | 782 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 236.0354° |
| argument of perigee: | 272.0234° |
| revolutions per day: | 14.31711029 |
| mean anomaly at epoch: | 88.0221° |
| orbit number at epoch: | 23111 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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