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 41029U 26145.58892845 +.00000000 +00000-0 +00000-0 0 00006
2 41029 0.0314 238.4484 0002698 324.5856 278.1275 1.00271435 02
| Epoch (UTC): | 25 May 2026 14:08:03 |
| Eccentricity: | 0.0002698 |
| inclination: | 0.0314° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 238.4484° |
| argument of perigee: | 324.5856° |
| revolutions per day: | 1.00271435 |
| mean anomaly at epoch: | 278.1275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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