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 26140.18713470 +.00000000 +00000-0 +13971-3 0 00006
2 22803 70.9904 220.3499 0014980 103.0829 257.1968 14.17242510 05
| Epoch (UTC): | 20 May 2026 04:29:28 |
| Eccentricity: | 0.0014980 |
| inclination: | 70.9904° |
| perigee height: | 824 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 220.3499° |
| argument of perigee: | 103.0829° |
| revolutions per day: | 14.17242510 |
| mean anomaly at epoch: | 257.1968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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