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 17526U 26072.70837645 +.00000000 +00000-0 +60794-4 0 00001
2 17526 82.9050 174.4236 0040747 34.8082 325.5728 13.77212967 08
| Epoch (UTC): | 13 March 2026 17:00:03 |
| Eccentricity: | 0.0040747 |
| inclination: | 82.9050° |
| perigee height: | 944 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 174.4236° |
| argument of perigee: | 34.8082° |
| revolutions per day: | 13.77212967 |
| mean anomaly at epoch: | 325.5728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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