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 52550U 26145.37194389 +.00000000 +00000-0 -57695-4 0 00009
2 52550 53.2123 144.8794 0001359 80.6091 279.5055 15.08825954 04
| Epoch (UTC): | 25 May 2026 08:55:35 |
| Eccentricity: | 0.0001359 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 144.8794° |
| argument of perigee: | 80.6091° |
| revolutions per day: | 15.08825954 |
| mean anomaly at epoch: | 279.5055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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