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 55796U 26145.66591078 +.00000000 +00000-0 -58943-4 0 00009
2 55796 87.9166 278.9614 0002357 101.6400 258.4998 13.20769930 02
| Epoch (UTC): | 25 May 2026 15:58:54 |
| Eccentricity: | 0.0002357 |
| inclination: | 87.9166° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9614° |
| argument of perigee: | 101.6400° |
| revolutions per day: | 13.20769930 |
| mean anomaly at epoch: | 258.4998° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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