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 22802U 26074.76873120 +.00000000 +00000-0 +49397-4 0 00006
2 22802 70.9273 89.0226 0020994 114.3208 246.0109 14.13647768 03
| Epoch (UTC): | 15 March 2026 18:26:58 |
| Eccentricity: | 0.0020994 |
| inclination: | 70.9273° |
| perigee height: | 832 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 89.0226° |
| argument of perigee: | 114.3208° |
| revolutions per day: | 14.13647768 |
| mean anomaly at epoch: | 246.0109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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