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 54167U 26145.41743863 +.00000000 +00000-0 +53329-4 0 00006
2 54167 53.2158 29.4554 0001293 94.6090 265.5050 15.08839305 06
| Epoch (UTC): | 25 May 2026 10:01:06 |
| Eccentricity: | 0.0001293 |
| inclination: | 53.2158° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 29.4554° |
| argument of perigee: | 94.6090° |
| revolutions per day: | 15.08839305 |
| mean anomaly at epoch: | 265.5050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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