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 54169U 26145.06136941 +.00000000 +00000-0 -56975-4 0 00003
2 54169 53.2145 20.8224 0001515 88.1413 271.9753 15.08846336 00
| Epoch (UTC): | 25 May 2026 01:28:22 |
| Eccentricity: | 0.0001515 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 20.8224° |
| argument of perigee: | 88.1413° |
| revolutions per day: | 15.08846336 |
| mean anomaly at epoch: | 271.9753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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