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 22314U 26145.40690994 +.00000000 +00000-0 +00000-0 0 00004
2 22314 14.1828 357.2298 0006798 180.1593 166.0476 1.00279720 09
| Epoch (UTC): | 25 May 2026 09:45:57 |
| Eccentricity: | 0.0006798 |
| inclination: | 14.1828° |
| perigee height: | 35756 km |
| apogee height: | 35813 km |
| right ascension of ascending node: | 357.2298° |
| argument of perigee: | 180.1593° |
| revolutions per day: | 1.00279720 |
| mean anomaly at epoch: | 166.0476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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