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 52126U 26145.53570101 +.00000000 +00000-0 +52845-3 0 00006
2 52126 53.2125 84.1451 0001498 92.0632 268.0532 15.08796572 09
| Epoch (UTC): | 25 May 2026 12:51:24 |
| Eccentricity: | 0.0001498 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.1451° |
| argument of perigee: | 92.0632° |
| revolutions per day: | 15.08796572 |
| mean anomaly at epoch: | 268.0532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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