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 52278U 26145.63873098 +.00000000 +00000-0 +17242-4 0 00009
2 52278 53.2130 123.6796 0001177 95.5801 264.5326 15.08835896 09
| Epoch (UTC): | 25 May 2026 15:19:46 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 123.6796° |
| argument of perigee: | 95.5801° |
| revolutions per day: | 15.08835896 |
| mean anomaly at epoch: | 264.5326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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