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 42846U 26066.40133029 +.00000000 +00000-0 +46892-3 0 00001
2 42846 97.3946 231.8191 0014397 100.3646 259.9205 15.05582031 05
| Epoch (UTC): | 07 March 2026 09:37:54 |
| Eccentricity: | 0.0014397 |
| inclination: | 97.3946° |
| perigee height: | 540 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 231.8191° |
| argument of perigee: | 100.3646° |
| revolutions per day: | 15.05582031 |
| mean anomaly at epoch: | 259.9205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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