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 26146.23111611 +.00000000 +00000-0 +00000-0 0 00004
2 22787 11.8874 3.6773 0007874 2.5961 349.4759 1.00278600 07
| Epoch (UTC): | 26 May 2026 05:32:48 |
| Eccentricity: | 0.0007874 |
| inclination: | 11.8874° |
| perigee height: | 35751 km |
| apogee height: | 35818 km |
| right ascension of ascending node: | 3.6773° |
| argument of perigee: | 2.5961° |
| revolutions per day: | 1.00278600 |
| mean anomaly at epoch: | 349.4759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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