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 52657U 26145.36878751 +.00000000 +00000-0 +33701-4 0 00009
2 52657 53.2133 170.2126 0001090 80.4152 279.6963 15.08835724 08
| Epoch (UTC): | 25 May 2026 08:51:03 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 170.2126° |
| argument of perigee: | 80.4152° |
| revolutions per day: | 15.08835724 |
| mean anomaly at epoch: | 279.6963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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