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 35525U 26087.59890992 +.00000000 +00000-0 +15140-3 0 00001
2 35525 82.5484 21.5045 0021621 105.3030 72.9173 13.83519995 06
| Epoch (UTC): | 28 March 2026 14:22:25 |
| Eccentricity: | 0.0021621 |
| inclination: | 82.5484° |
| perigee height: | 936 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 21.5045° |
| argument of perigee: | 105.3030° |
| revolutions per day: | 13.83519995 |
| mean anomaly at epoch: | 72.9173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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