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 54840U 26145.46449867 +.00000000 +00000-0 +45570-4 0 00005
2 54840 43.0036 59.1874 0000912 262.4623 97.6125 15.27585551 04
| Epoch (UTC): | 25 May 2026 11:08:52 |
| Eccentricity: | 0.0000912 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 59.1874° |
| argument of perigee: | 262.4623° |
| revolutions per day: | 15.27585551 |
| mean anomaly at epoch: | 97.6125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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