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 17528U 26064.98898376 +.00000000 +00000-0 +25442-3 0 00002
2 17528 97.4035 70.9548 0144962 25.3766 335.4461 14.54475721 07
| Epoch (UTC): | 05 March 2026 23:44:08 |
| Eccentricity: | 0.0144962 |
| inclination: | 97.4035° |
| perigee height: | 608 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 70.9548° |
| argument of perigee: | 25.3766° |
| revolutions per day: | 14.54475721 |
| mean anomaly at epoch: | 335.4461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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