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 52375U 26145.46208660 +.00000000 +00000-0 +14047-4 0 00005
2 52375 53.2102 204.4767 0001182 93.3076 266.8051 15.08833281 04
| Epoch (UTC): | 25 May 2026 11:05:24 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.2102° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 204.4767° |
| argument of perigee: | 93.3076° |
| revolutions per day: | 15.08833281 |
| mean anomaly at epoch: | 266.8051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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