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 22888U 26106.84580970 +.00000000 +00000-0 +42711-4 0 00006
2 22888 82.9478 126.6143 0048074 0.3629 174.3140 13.75171912 01
| Epoch (UTC): | 16 April 2026 20:17:57 |
| Eccentricity: | 0.0048074 |
| inclination: | 82.9478° |
| perigee height: | 946 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 126.6143° |
| argument of perigee: | 0.3629° |
| revolutions per day: | 13.75171912 |
| mean anomaly at epoch: | 174.3140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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