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 52273U 26145.29472911 +.00000000 +00000-0 -11971-3 0 00008
2 52273 53.2138 115.6078 0001121 99.7578 260.3541 15.08856387 03
| Epoch (UTC): | 25 May 2026 07:04:24 |
| Eccentricity: | 0.0001121 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 115.6078° |
| argument of perigee: | 99.7578° |
| revolutions per day: | 15.08856387 |
| mean anomaly at epoch: | 260.3541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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