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 18958U 26162.50292749 +.00000000 +00000-0 +13599-3 0 00009
2 18958 82.5116 158.0641 0002880 208.9825 151.1250 15.18677989 09
| Epoch (UTC): | 11 June 2026 12:04:12 |
| Eccentricity: | 0.0002880 |
| inclination: | 82.5116° |
| perigee height: | 508 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 158.0641° |
| argument of perigee: | 208.9825° |
| revolutions per day: | 15.18677989 |
| mean anomaly at epoch: | 151.1250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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