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 22220U 26159.00323513 +.00000000 +00000-0 -76975-4 0 00000
2 22220 71.0007 358.1286 0014450 310.6399 161.6193 14.16872143 07
| Epoch (UTC): | 08 June 2026 00:04:39 |
| Eccentricity: | 0.0014450 |
| inclination: | 71.0007° |
| perigee height: | 826 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 358.1286° |
| argument of perigee: | 310.6399° |
| revolutions per day: | 14.16872143 |
| mean anomaly at epoch: | 161.6193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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