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 52990U 26145.31720022 +.00000000 +00000-0 +72189-4 0 00004
2 52990 53.2122 120.1280 0001059 75.6237 284.4872 15.08841692 00
| Epoch (UTC): | 25 May 2026 07:36:46 |
| Eccentricity: | 0.0001059 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 120.1280° |
| argument of perigee: | 75.6237° |
| revolutions per day: | 15.08841692 |
| mean anomaly at epoch: | 284.4872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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