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 52622U 26145.40735178 +.00000000 +00000-0 +30950-4 0 00004
2 52622 53.2122 299.7210 0001071 86.8609 273.2506 15.08832663 07
| Epoch (UTC): | 25 May 2026 09:46:35 |
| Eccentricity: | 0.0001071 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 299.7210° |
| argument of perigee: | 86.8609° |
| revolutions per day: | 15.08832663 |
| mean anomaly at epoch: | 273.2506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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