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 25724U 26146.15014433 +.00000000 +00000-0 +12862-2 0 00004
2 25724 28.2257 36.2529 2131889 131.6175 248.7571 9.37509865 07
| Epoch (UTC): | 26 May 2026 03:36:12 |
| Eccentricity: | 0.2131889 |
| inclination: | 28.2257° |
| perigee height: | 1097 km |
| apogee height: | 5148 km |
| right ascension of ascending node: | 36.2529° |
| argument of perigee: | 131.6175° |
| revolutions per day: | 9.37509865 |
| mean anomaly at epoch: | 248.7571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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