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 43631U 26087.71559483 +.00000000 +00000-0 +18441-2 0 00005
2 43631 100.5948 261.6654 0187389 39.3935 322.0677 13.91301531 08
| Epoch (UTC): | 28 March 2026 17:10:27 |
| Eccentricity: | 0.0187389 |
| inclination: | 100.5948° |
| perigee height: | 787 km |
| apogee height: | 1061 km |
| right ascension of ascending node: | 261.6654° |
| argument of perigee: | 39.3935° |
| revolutions per day: | 13.91301531 |
| mean anomaly at epoch: | 322.0677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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