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 39222U 26023.33442175 +.00000000 +00000-0 +00000-0 0 00003
2 39222 0.0177 76.3619 0000301 228.1804 163.3283 1.00272238 07
| Epoch (UTC): | 23 January 2026 08:01:34 |
| Eccentricity: | 0.0000301 |
| inclination: | 0.0177° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 76.3619° |
| argument of perigee: | 228.1804° |
| revolutions per day: | 1.00272238 |
| mean anomaly at epoch: | 163.3283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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