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 52536U 26145.41240591 +.00000000 +00000-0 +11450-3 0 00002
2 52536 53.2119 144.6976 0001174 73.8790 286.2331 15.08849989 04
| Epoch (UTC): | 25 May 2026 09:53:51 |
| Eccentricity: | 0.0001174 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 144.6976° |
| argument of perigee: | 73.8790° |
| revolutions per day: | 15.08849989 |
| mean anomaly at epoch: | 286.2331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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