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 52987U 26145.32454389 +.00000000 +00000-0 +60608-4 0 00004
2 52987 53.2135 120.0929 0001191 77.5974 282.5152 15.08843722 01
| Epoch (UTC): | 25 May 2026 07:47:20 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 120.0929° |
| argument of perigee: | 77.5974° |
| revolutions per day: | 15.08843722 |
| mean anomaly at epoch: | 282.5152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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