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 18960U 26150.14717780 +.00000000 +00000-0 +19429-3 0 00004
2 18960 98.8510 205.5001 0013120 257.6721 118.7992 13.97167714 00
| Epoch (UTC): | 30 May 2026 03:31:56 |
| Eccentricity: | 0.0013120 |
| inclination: | 98.8510° |
| perigee height: | 894 km |
| apogee height: | 913 km |
| right ascension of ascending node: | 205.5001° |
| argument of perigee: | 257.6721° |
| revolutions per day: | 13.97167714 |
| mean anomaly at epoch: | 118.7992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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