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 41310U 26145.58554845 +.00000000 +00000-0 +00000-0 0 00004
2 41310 0.0833 78.2056 0002460 307.1738 77.5926 1.00273904 06
| Epoch (UTC): | 25 May 2026 14:03:11 |
| Eccentricity: | 0.0002460 |
| inclination: | 0.0833° |
| perigee height: | 35776 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 78.2056° |
| argument of perigee: | 307.1738° |
| revolutions per day: | 1.00273904 |
| mean anomaly at epoch: | 77.5926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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