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 26074.26456779 +.00000000 +00000-0 +77433-4 0 00001
2 22803 70.9930 359.3708 0018205 208.3331 151.6804 14.17231741 02
| Epoch (UTC): | 15 March 2026 06:20:58 |
| Eccentricity: | 0.0018205 |
| inclination: | 70.9930° |
| perigee height: | 822 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 359.3708° |
| argument of perigee: | 208.3331° |
| revolutions per day: | 14.17231741 |
| mean anomaly at epoch: | 151.6804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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