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 22803U 26020.69328916 +.00000000 +00000-0 +68869-4 0 00003
2 22803 70.9908 112.3451 0019540 281.7820 78.1112 14.17223643 07
| Epoch (UTC): | 20 January 2026 16:38:20 |
| Eccentricity: | 0.0019540 |
| inclination: | 70.9908° |
| perigee height: | 821 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 112.3451° |
| argument of perigee: | 281.7820° |
| revolutions per day: | 14.17223643 |
| mean anomaly at epoch: | 78.1112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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