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 26905U 01040A 23086.96610341 0.00000500 00000-0 36070-3 0 03
2 26905 63.3870 35.3982 0556272 5.1475 354.8525 13.40899206 04
| Epoch (UTC): | 27 March 2023 23:11:11 |
| Eccentricity: | 0.0556272 |
| inclination: | 63.3870° |
| perigee height: | 689 km |
| apogee height: | 1522 km |
| right ascension of ascending node: | 35.3982° |
| argument of perigee: | 5.1475° |
| revolutions per day: | 13.40899206 |
| mean anomaly at epoch: | 354.8525° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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