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 43632U 26145.59265514 +.00000000 +00000-0 +00000-0 0 00006
2 43632 0.0185 315.8802 0001558 108.7712 76.9867 1.00271564 05
| Epoch (UTC): | 25 May 2026 14:13:25 |
| Eccentricity: | 0.0001558 |
| inclination: | 0.0185° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 315.8802° |
| argument of perigee: | 108.7712° |
| revolutions per day: | 1.00271564 |
| mean anomaly at epoch: | 76.9867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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