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 54061U 26145.48780279 +.00000000 +00000-0 +44461-4 0 00005
2 54061 53.2125 323.9706 0001178 91.6184 268.4943 15.08837962 07
| Epoch (UTC): | 25 May 2026 11:42:26 |
| Eccentricity: | 0.0001178 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 323.9706° |
| argument of perigee: | 91.6184° |
| revolutions per day: | 15.08837962 |
| mean anomaly at epoch: | 268.4943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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