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 35937U 09052A 25358.75803544 0.00000050 00000-0 20859-3 0 07
2 35937 57.9868 215.7876 0015979 19.3135 340.6864 12.83571683 06
| Epoch (UTC): | 24 December 2025 18:11:34 |
| Eccentricity: | 0.0015979 |
| inclination: | 57.9868° |
| perigee height: | 1315 km |
| apogee height: | 1339 km |
| right ascension of ascending node: | 215.7876° |
| argument of perigee: | 19.3135° |
| revolutions per day: | 12.83571683 |
| mean anomaly at epoch: | 340.6864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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