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 52339U 26145.49700213 +.00000000 +00000-0 -39228-4 0 00008
2 52339 53.2128 223.9607 0001464 86.8805 273.2355 15.08843173 01
| Epoch (UTC): | 25 May 2026 11:55:40 |
| Eccentricity: | 0.0001464 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 223.9607° |
| argument of perigee: | 86.8805° |
| revolutions per day: | 15.08843173 |
| mean anomaly at epoch: | 273.2355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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