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 26072.92352330 +.00000000 +00000-0 +33447-4 0 00007
2 22803 70.9929 2.1985 0018291 210.3056 149.7012 14.17231457 05
| Epoch (UTC): | 13 March 2026 22:09:52 |
| Eccentricity: | 0.0018291 |
| inclination: | 70.9929° |
| perigee height: | 822 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 2.1985° |
| argument of perigee: | 210.3056° |
| revolutions per day: | 14.17231457 |
| mean anomaly at epoch: | 149.7012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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