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 52662U 26145.44874914 +.00000000 +00000-0 +46140-4 0 00002
2 52662 53.2121 169.5370 0000963 66.0131 294.0962 15.08838077 02
| Epoch (UTC): | 25 May 2026 10:46:11 |
| Eccentricity: | 0.0000963 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 169.5370° |
| argument of perigee: | 66.0131° |
| revolutions per day: | 15.08838077 |
| mean anomaly at epoch: | 294.0962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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