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 26129.52944435 +.00000000 +00000-0 -78195-4 0 00009
2 22803 70.9906 242.8238 0015163 121.6496 238.6109 14.17242236 03
| Epoch (UTC): | 09 May 2026 12:42:23 |
| Eccentricity: | 0.0015163 |
| inclination: | 70.9906° |
| perigee height: | 824 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 242.8238° |
| argument of perigee: | 121.6496° |
| revolutions per day: | 14.17242236 |
| mean anomaly at epoch: | 238.6109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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