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 is defined by the following mean orbital elements,
1 35938U 09052B 26010.73325737 0.00000040 00000-0 18803-3 0 00
2 35938 57.9848 235.1672 0021008 69.8134 290.1866 12.74862161 09
| Epoch (UTC): | 10 January 2026 17:35:53 |
| Eccentricity: | 0.0021008 |
| inclination: | 57.9848° |
| perigee height: | 1346 km |
| apogee height: | 1378 km |
| right ascension of ascending node: | 235.1672° |
| argument of perigee: | 69.8134° |
| revolutions per day: | 12.74862161 |
| mean anomaly at epoch: | 290.1866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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