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 17360U 26156.49322007 +.00000000 +00000-0 +10014-3 0 00006
2 17360 82.9190 346.1081 0033060 34.0072 26.1985 13.77057957 01
| Epoch (UTC): | 05 June 2026 11:50:14 |
| Eccentricity: | 0.0033060 |
| inclination: | 82.9190° |
| perigee height: | 950 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 346.1081° |
| argument of perigee: | 34.0072° |
| revolutions per day: | 13.77057957 |
| mean anomaly at epoch: | 26.1985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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