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 22626U 26040.15151178 +.00000000 +00000-0 +16147-3 0 00004
2 22626 82.5191 294.0123 0017620 45.1177 315.1472 14.96429420 02
| Epoch (UTC): | 09 February 2026 03:38:10 |
| Eccentricity: | 0.0017620 |
| inclination: | 82.5191° |
| perigee height: | 566 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 294.0123° |
| argument of perigee: | 45.1177° |
| revolutions per day: | 14.96429420 |
| mean anomaly at epoch: | 315.1472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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