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 25078.73203438 0.00001000 00000-0 56102-3 0 00
2 26905 63.3870 338.9869 0622344 9.2465 350.7534 13.41412030 00
| Epoch (UTC): | 19 March 2025 17:34:07 |
| Eccentricity: | 0.0622344 |
| inclination: | 63.3870° |
| perigee height: | 638 km |
| apogee height: | 1569 km |
| right ascension of ascending node: | 338.9869° |
| argument of perigee: | 9.2465° |
| revolutions per day: | 13.41412030 |
| mean anomaly at epoch: | 350.7534° |
| 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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