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 22077U 26154.63729939 +.00000000 +00000-0 +43973-4 0 00007
2 22077 66.0860 309.4958 0015120 286.2398 164.4179 12.86612432 08
| Epoch (UTC): | 03 June 2026 15:17:42 |
| Eccentricity: | 0.0015120 |
| inclination: | 66.0860° |
| perigee height: | 1303 km |
| apogee height: | 1327 km |
| right ascension of ascending node: | 309.4958° |
| argument of perigee: | 286.2398° |
| revolutions per day: | 12.86612432 |
| mean anomaly at epoch: | 164.4179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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