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 54223U 26142.26584559 +.00000000 +00000-0 +00000-0 0 00008
2 54223 63.2865 283.7868 7054885 269.6534 16.6198 2.00574391 04
| Epoch (UTC): | 22 May 2026 06:22:49 |
| Eccentricity: | 0.7054885 |
| inclination: | 63.2865° |
| perigee height: | 1444 km |
| apogee height: | 38919 km |
| right ascension of ascending node: | 283.7868° |
| argument of perigee: | 269.6534° |
| revolutions per day: | 2.00574391 |
| mean anomaly at epoch: | 16.6198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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