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 22028U 26150.40513858 +.00000000 +00000-0 +00000-0 0 00005
2 22028 14.7321 5.5692 0007149 271.1676 288.7247 0.99081522 06
| Epoch (UTC): | 30 May 2026 09:43:23 |
| Eccentricity: | 0.0007149 |
| inclination: | 14.7321° |
| perigee height: | 36093 km |
| apogee height: | 36154 km |
| right ascension of ascending node: | 5.5692° |
| argument of perigee: | 271.1676° |
| revolutions per day: | 0.99081522 |
| mean anomaly at epoch: | 288.7247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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