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 19460U 26162.58000830 +.00000000 +00000-0 +44810-4 0 00005
2 19460 84.9860 116.3311 0004800 111.4003 248.7704 14.34442982 08
| Epoch (UTC): | 11 June 2026 13:55:12 |
| Eccentricity: | 0.0004800 |
| inclination: | 84.9860° |
| perigee height: | 773 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 116.3311° |
| argument of perigee: | 111.4003° |
| revolutions per day: | 14.34442982 |
| mean anomaly at epoch: | 248.7704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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