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 26072.00596647 +.00000000 +00000-0 +74946-5 0 00007
2 22803 70.9929 4.1331 0018342 211.6638 148.3383 14.17231380 00
| Epoch (UTC): | 13 March 2026 00:08:35 |
| Eccentricity: | 0.0018342 |
| inclination: | 70.9929° |
| perigee height: | 822 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 4.1331° |
| argument of perigee: | 211.6638° |
| revolutions per day: | 14.17231380 |
| mean anomaly at epoch: | 148.3383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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