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 18710U 26088.09111005 +.00000000 +00000-0 +17906-3 0 00007
2 18710 82.9073 96.1559 0024206 129.9699 290.0580 13.76294932 02
| Epoch (UTC): | 29 March 2026 02:11:11 |
| Eccentricity: | 0.0024206 |
| inclination: | 82.9073° |
| perigee height: | 959 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 96.1559° |
| argument of perigee: | 129.9699° |
| revolutions per day: | 13.76294932 |
| mean anomaly at epoch: | 290.0580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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