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 53641U 26145.63731470 +.00000000 +00000-0 +13285-3 0 00003
2 53641 53.2137 238.5518 0001670 69.6529 290.4642 15.08852630 00
| Epoch (UTC): | 25 May 2026 15:17:43 |
| Eccentricity: | 0.0001670 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 238.5518° |
| argument of perigee: | 69.6529° |
| revolutions per day: | 15.08852630 |
| mean anomaly at epoch: | 290.4642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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