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 54053U 26145.01544954 +.00000000 +00000-0 +27752-4 0 00007
2 54053 53.2149 1.6871 0001347 89.0165 271.0982 15.08840843 00
| Epoch (UTC): | 25 May 2026 00:22:14 |
| Eccentricity: | 0.0001347 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 1.6871° |
| argument of perigee: | 89.0165° |
| revolutions per day: | 15.08840843 |
| mean anomaly at epoch: | 271.0982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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