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 52679U 26145.45334966 +.00000000 +00000-0 +13675-4 0 00006
2 52679 53.2104 159.5157 0001186 71.2956 288.8165 15.08852345 04
| Epoch (UTC): | 25 May 2026 10:52:49 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.2104° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 159.5157° |
| argument of perigee: | 71.2956° |
| revolutions per day: | 15.08852345 |
| mean anomaly at epoch: | 288.8165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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