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 26074.23405012 +.00000000 +00000-0 +43800-4 0 00009
2 17526 82.9048 173.2830 0040665 30.6542 329.6978 13.77213075 09
| Epoch (UTC): | 15 March 2026 05:37:01 |
| Eccentricity: | 0.0040665 |
| inclination: | 82.9048° |
| perigee height: | 944 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 173.2830° |
| argument of perigee: | 30.6542° |
| revolutions per day: | 13.77213075 |
| mean anomaly at epoch: | 329.6978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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