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 52269U 26145.33328803 +.00000000 +00000-0 +50960-4 0 00009
2 52269 53.2127 125.0554 0001068 85.7808 274.3306 15.08839379 07
| Epoch (UTC): | 25 May 2026 07:59:56 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 125.0554° |
| argument of perigee: | 85.7808° |
| revolutions per day: | 15.08839379 |
| mean anomaly at epoch: | 274.3306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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