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 22723U 26150.42633646 +.00000000 +00000-0 +00000-0 0 00007
2 22723 13.7101 13.2308 0007312 358.8506 1.6613 0.99728029 09
| Epoch (UTC): | 30 May 2026 10:13:55 |
| Eccentricity: | 0.0007312 |
| inclination: | 13.7101° |
| perigee height: | 35909 km |
| apogee height: | 35971 km |
| right ascension of ascending node: | 13.2308° |
| argument of perigee: | 358.8506° |
| revolutions per day: | 0.99728029 |
| mean anomaly at epoch: | 1.6613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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