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 55169U 26145.30517346 +.00000000 +00000-0 -10822-2 0 00002
2 55169 87.8959 355.2035 0002465 91.1961 268.9450 13.12443044 01
| Epoch (UTC): | 25 May 2026 07:19:26 |
| Eccentricity: | 0.0002465 |
| inclination: | 87.8959° |
| perigee height: | 1212 km |
| apogee height: | 1216 km |
| right ascension of ascending node: | 355.2035° |
| argument of perigee: | 91.1961° |
| revolutions per day: | 13.12443044 |
| mean anomaly at epoch: | 268.9450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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