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 53757U 26145.49866079 +.00000000 +00000-0 +49462-4 0 00006
2 53757 53.5309 149.0757 0008268 287.3806 72.6265 14.61225495 02
| Epoch (UTC): | 25 May 2026 11:58:04 |
| Eccentricity: | 0.0008268 |
| inclination: | 53.5309° |
| perigee height: | 683 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 149.0757° |
| argument of perigee: | 287.3806° |
| revolutions per day: | 14.61225495 |
| mean anomaly at epoch: | 72.6265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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