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 53155U 26145.36318448 +.00000000 +00000-0 +60556-4 0 00003
2 53155 53.2131 179.9194 0001139 64.7865 295.3245 15.08843732 07
| Epoch (UTC): | 25 May 2026 08:42:59 |
| Eccentricity: | 0.0001139 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 179.9194° |
| argument of perigee: | 64.7865° |
| revolutions per day: | 15.08843732 |
| mean anomaly at epoch: | 295.3245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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