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 22487U 26053.68411779 +.00000000 +00000-0 +49214-4 0 00009
2 22487 82.9407 267.5054 0039295 76.1586 349.9341 13.76029558 04
| Epoch (UTC): | 22 February 2026 16:25:07 |
| Eccentricity: | 0.0039295 |
| inclination: | 82.9407° |
| perigee height: | 949 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 267.5054° |
| argument of perigee: | 76.1586° |
| revolutions per day: | 13.76029558 |
| mean anomaly at epoch: | 349.9341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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