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 26088.18247779 +.00000000 +00000-0 -42482-4 0 00005
2 22220 70.9997 147.3158 0010707 59.9120 3.2767 14.16863910 05
| Epoch (UTC): | 29 March 2026 04:22:46 |
| Eccentricity: | 0.0010707 |
| inclination: | 70.9997° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 147.3158° |
| argument of perigee: | 59.9120° |
| revolutions per day: | 14.16863910 |
| mean anomaly at epoch: | 3.2767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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