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 41729U 26145.32704986 +.00000000 +00000-0 +00000-0 0 00003
2 41729 0.0163 321.1038 0001194 106.6212 76.8640 1.00268134 02
| Epoch (UTC): | 25 May 2026 07:50:57 |
| Eccentricity: | 0.0001194 |
| inclination: | 0.0163° |
| perigee height: | 35783 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 321.1038° |
| argument of perigee: | 106.6212° |
| revolutions per day: | 1.00268134 |
| mean anomaly at epoch: | 76.8640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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