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 65504U 26145.07371338 +.00000000 +00000-0 +58246-3 0 00001
2 65504 53.1603 275.5729 0001159 87.0135 273.1000 15.34397382 05
| Epoch (UTC): | 25 May 2026 01:46:08 |
| Eccentricity: | 0.0001159 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 275.5729° |
| argument of perigee: | 87.0135° |
| revolutions per day: | 15.34397382 |
| mean anomaly at epoch: | 273.1000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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