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 24726U 26103.84892139 +.00000000 +00000-0 +17754-3 0 00007
2 24726 82.5976 304.5122 0004292 230.3423 129.7290 12.61392722 06
| Epoch (UTC): | 13 April 2026 20:22:26 |
| Eccentricity: | 0.0004292 |
| inclination: | 82.5976° |
| perigee height: | 1414 km |
| apogee height: | 1421 km |
| right ascension of ascending node: | 304.5122° |
| argument of perigee: | 230.3423° |
| revolutions per day: | 12.61392722 |
| mean anomaly at epoch: | 129.7290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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