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 26106.61693939 +.00000000 +00000-0 -20635-4 0 00003
2 22077 66.0863 50.0958 0014156 297.9051 234.2699 12.86610890 02
| Epoch (UTC): | 16 April 2026 14:48:23 |
| Eccentricity: | 0.0014156 |
| inclination: | 66.0863° |
| perigee height: | 1304 km |
| apogee height: | 1326 km |
| right ascension of ascending node: | 50.0958° |
| argument of perigee: | 297.9051° |
| revolutions per day: | 12.86610890 |
| mean anomaly at epoch: | 234.2699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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