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 22638U 26146.27942340 +.00000000 +00000-0 +62802-4 0 00006
2 22638 69.9216 346.5955 0059732 190.9970 168.9855 14.33661169 06
| Epoch (UTC): | 26 May 2026 06:42:22 |
| Eccentricity: | 0.0059732 |
| inclination: | 69.9216° |
| perigee height: | 737 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 346.5955° |
| argument of perigee: | 190.9970° |
| revolutions per day: | 14.33661169 |
| mean anomaly at epoch: | 168.9855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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