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 52544U 26145.41746934 +.00000000 +00000-0 +19250-3 0 00009
2 52544 53.2133 149.6846 0001343 93.1397 266.9749 15.08826682 09
| Epoch (UTC): | 25 May 2026 10:01:09 |
| Eccentricity: | 0.0001343 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 149.6846° |
| argument of perigee: | 93.1397° |
| revolutions per day: | 15.08826682 |
| mean anomaly at epoch: | 266.9749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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