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 26064.94784178 +.00000000 +00000-0 -32481-4 0 00007
2 22803 70.9923 19.0160 0018715 221.8806 138.0887 14.17232136 08
| Epoch (UTC): | 05 March 2026 22:44:53 |
| Eccentricity: | 0.0018715 |
| inclination: | 70.9923° |
| perigee height: | 821 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 19.0160° |
| argument of perigee: | 221.8806° |
| revolutions per day: | 14.17232136 |
| mean anomaly at epoch: | 138.0887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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