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 52281U 26145.24592940 +.00000000 +00000-0 -88949-4 0 00007
2 52281 53.2130 125.4427 0001398 39.6040 320.5054 15.08848670 08
| Epoch (UTC): | 25 May 2026 05:54:08 |
| Eccentricity: | 0.0001398 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 125.4427° |
| argument of perigee: | 39.6040° |
| revolutions per day: | 15.08848670 |
| mean anomaly at epoch: | 320.5054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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