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 22787U 26140.26989301 +.00000000 +00000-0 +00000-0 0 00000
2 22787 11.8855 3.7104 0008307 1.2654 358.7548 1.00275748 01
| Epoch (UTC): | 20 May 2026 06:28:38 |
| Eccentricity: | 0.0008307 |
| inclination: | 11.8855° |
| perigee height: | 35750 km |
| apogee height: | 35821 km |
| right ascension of ascending node: | 3.7104° |
| argument of perigee: | 1.2654° |
| revolutions per day: | 1.00275748 |
| mean anomaly at epoch: | 358.7548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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