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 17242U 26073.33587237 +.00000000 +00000-0 +84993-5 0 00003
2 17242 82.5351 5.6367 0016351 104.0775 17.5115 13.83390702 05
| Epoch (UTC): | 14 March 2026 08:03:39 |
| Eccentricity: | 0.0016351 |
| inclination: | 82.5351° |
| perigee height: | 940 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 5.6367° |
| argument of perigee: | 104.0775° |
| revolutions per day: | 13.83390702 |
| mean anomaly at epoch: | 17.5115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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