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 26075.68707227 +.00000000 +00000-0 +50249-4 0 00007
2 17526 82.9048 172.1970 0040580 26.6455 333.6776 13.77213247 08
| Epoch (UTC): | 16 March 2026 16:29:23 |
| Eccentricity: | 0.0040580 |
| inclination: | 82.9048° |
| perigee height: | 944 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 172.1970° |
| argument of perigee: | 26.6455° |
| revolutions per day: | 13.77213247 |
| mean anomaly at epoch: | 333.6776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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