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 66922U 26145.41327127 +.00000000 +00000-0 +53904-4 0 00008
2 66922 50.0079 227.4345 0001068 212.6083 147.4724 13.29325228 08
| Epoch (UTC): | 25 May 2026 09:55:06 |
| Eccentricity: | 0.0001068 |
| inclination: | 50.0079° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 227.4345° |
| argument of perigee: | 212.6083° |
| revolutions per day: | 13.29325228 |
| mean anomaly at epoch: | 147.4724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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