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 22988U 26138.48688876 +.00000000 +00000-0 +00000-0 0 00007
2 22988 17.5844 28.0146 0001276 252.4339 301.8056 0.98723969 01
| Epoch (UTC): | 18 May 2026 11:41:07 |
| Eccentricity: | 0.0001276 |
| inclination: | 17.5844° |
| perigee height: | 36221 km |
| apogee height: | 36232 km |
| right ascension of ascending node: | 28.0146° |
| argument of perigee: | 252.4339° |
| revolutions per day: | 0.98723969 |
| mean anomaly at epoch: | 301.8056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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