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 41471U 26145.54280769 +.00000000 +00000-0 +00000-0 0 00009
2 41471 0.0180 328.2345 0001164 103.6255 160.6762 1.00270471 09
| Epoch (UTC): | 25 May 2026 13:01:38 |
| Eccentricity: | 0.0001164 |
| inclination: | 0.0180° |
| perigee height: | 35782 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 328.2345° |
| argument of perigee: | 103.6255° |
| revolutions per day: | 1.00270471 |
| mean anomaly at epoch: | 160.6762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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