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 43636U 26145.49223816 +.00000000 +00000-0 +10706-3 0 00005
2 43636 97.8737 170.3955 0008435 182.4850 177.6311 14.59965785 08
| Epoch (UTC): | 25 May 2026 11:48:49 |
| Eccentricity: | 0.0008435 |
| inclination: | 97.8737° |
| perigee height: | 687 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 170.3955° |
| argument of perigee: | 182.4850° |
| revolutions per day: | 14.59965785 |
| mean anomaly at epoch: | 177.6311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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