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 26053.71930619 +.00000000 +00000-0 +59292-4 0 00004
2 22888 82.9548 165.9234 0049046 145.6799 328.7261 13.75166384 03
| Epoch (UTC): | 22 February 2026 17:15:48 |
| Eccentricity: | 0.0049046 |
| inclination: | 82.9548° |
| perigee height: | 945 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 165.9234° |
| argument of perigee: | 145.6799° |
| revolutions per day: | 13.75166384 |
| mean anomaly at epoch: | 328.7261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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