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 25933U 26065.59965089 +.00000000 +00000-0 +00000-0 0 00005
2 25933 51.5551 299.9561 0106417 171.7421 195.4559 2.00567698 00
| Epoch (UTC): | 06 March 2026 14:23:29 |
| Eccentricity: | 0.0106417 |
| inclination: | 51.5551° |
| perigee height: | 19899 km |
| apogee height: | 20464 km |
| right ascension of ascending node: | 299.9561° |
| argument of perigee: | 171.7421° |
| revolutions per day: | 2.00567698 |
| mean anomaly at epoch: | 195.4559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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