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 52706U 26145.38803280 +.00000000 +00000-0 +28515-4 0 00008
2 52706 53.2114 149.8071 0001147 57.9105 302.1999 15.08834409 03
| Epoch (UTC): | 25 May 2026 09:18:46 |
| Eccentricity: | 0.0001147 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 149.8071° |
| argument of perigee: | 57.9105° |
| revolutions per day: | 15.08834409 |
| mean anomaly at epoch: | 302.1999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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