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 26139.62248941 +.00000000 +00000-0 +13650-3 0 00003
2 22803 70.9904 221.5406 0014991 104.0760 256.2031 14.17242224 06
| Epoch (UTC): | 19 May 2026 14:56:23 |
| Eccentricity: | 0.0014991 |
| inclination: | 70.9904° |
| perigee height: | 824 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 221.5406° |
| argument of perigee: | 104.0760° |
| revolutions per day: | 14.17242224 |
| mean anomaly at epoch: | 256.2031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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