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 22078U 26053.62088485 +.00000000 +00000-0 +15231-3 0 00004
2 22078 66.0854 148.5663 0013913 310.2623 49.7178 12.86850011 05
| Epoch (UTC): | 22 February 2026 14:54:04 |
| Eccentricity: | 0.0013913 |
| inclination: | 66.0854° |
| perigee height: | 1303 km |
| apogee height: | 1325 km |
| right ascension of ascending node: | 148.5663° |
| argument of perigee: | 310.2623° |
| revolutions per day: | 12.86850011 |
| mean anomaly at epoch: | 49.7178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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