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 41105U 26145.08180250 +.00000000 +00000-0 +00000-0 0 00006
2 41105 6.6386 70.8029 0001449 264.6302 282.1844 1.00271753 04
| Epoch (UTC): | 25 May 2026 01:57:47 |
| Eccentricity: | 0.0001449 |
| inclination: | 6.6386° |
| perigee height: | 35781 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 70.8029° |
| argument of perigee: | 264.6302° |
| revolutions per day: | 1.00271753 |
| mean anomaly at epoch: | 282.1844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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