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 52695U 26145.46205970 +.00000000 +00000-0 +36163-4 0 00004
2 52695 53.2129 164.2703 0001181 81.2631 278.8495 15.08841799 01
| Epoch (UTC): | 25 May 2026 11:05:21 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.2703° |
| argument of perigee: | 81.2631° |
| revolutions per day: | 15.08841799 |
| mean anomaly at epoch: | 278.8495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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