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 52605U 26145.44142838 +.00000000 +00000-0 -16082-3 0 00004
2 52605 53.2168 299.3461 0001521 91.6411 268.4756 15.08811984 03
| Epoch (UTC): | 25 May 2026 10:35:39 |
| Eccentricity: | 0.0001521 |
| inclination: | 53.2168° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 299.3461° |
| argument of perigee: | 91.6411° |
| revolutions per day: | 15.08811984 |
| mean anomaly at epoch: | 268.4756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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