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 54795U 26145.14190368 +.00000000 +00000-0 -10332-3 0 00006
2 54795 53.2135 45.7393 0001497 83.4060 276.7103 15.08846732 04
| Epoch (UTC): | 25 May 2026 03:24:20 |
| Eccentricity: | 0.0001497 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 45.7393° |
| argument of perigee: | 83.4060° |
| revolutions per day: | 15.08846732 |
| mean anomaly at epoch: | 276.7103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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