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 42950U 26145.36628384 +.00000000 +00000-0 +00000-0 0 00001
2 42950 0.0098 298.3886 0002467 138.6231 279.8134 1.00271647 08
| Epoch (UTC): | 25 May 2026 08:47:26 |
| Eccentricity: | 0.0002467 |
| inclination: | 0.0098° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 298.3886° |
| argument of perigee: | 138.6231° |
| revolutions per day: | 1.00271647 |
| mean anomaly at epoch: | 279.8134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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