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 18986U 26070.85354119 +.00000000 +00000-0 +10946-3 0 00009
2 18986 82.9578 190.0025 0040358 261.1708 98.4880 13.78932995 08
| Epoch (UTC): | 11 March 2026 20:29:05 |
| Eccentricity: | 0.0040358 |
| inclination: | 82.9578° |
| perigee height: | 938 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 190.0025° |
| argument of perigee: | 261.1708° |
| revolutions per day: | 13.78932995 |
| mean anomaly at epoch: | 98.4880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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