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 52333U 26145.49334885 +.00000000 +00000-0 +15924-3 0 00005
2 52333 53.2136 224.3332 0001484 92.8398 267.2764 15.08859301 07
| Epoch (UTC): | 25 May 2026 11:50:25 |
| Eccentricity: | 0.0001484 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 224.3332° |
| argument of perigee: | 92.8398° |
| revolutions per day: | 15.08859301 |
| mean anomaly at epoch: | 267.2764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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