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 22081U 26088.15232669 +.00000000 +00000-0 +99363-4 0 00008
2 22081 74.0449 334.1597 0036320 238.0759 121.6859 14.34835151 00
| Epoch (UTC): | 29 March 2026 03:39:21 |
| Eccentricity: | 0.0036320 |
| inclination: | 74.0449° |
| perigee height: | 750 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 334.1597° |
| argument of perigee: | 238.0759° |
| revolutions per day: | 14.34835151 |
| mean anomaly at epoch: | 121.6859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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