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 26156.26692964 +.00000000 +00000-0 +10584-2 0 00007
2 25724 28.2290 12.0435 2131834 171.1830 193.3163 9.37511951 00
| Epoch (UTC): | 05 June 2026 06:24:22 |
| Eccentricity: | 0.2131834 |
| inclination: | 28.2290° |
| perigee height: | 1097 km |
| apogee height: | 5148 km |
| right ascension of ascending node: | 12.0435° |
| argument of perigee: | 171.1830° |
| revolutions per day: | 9.37511951 |
| mean anomaly at epoch: | 193.3163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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