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 53153U 26145.37054535 +.00000000 +00000-0 -22040-4 0 00003
2 53153 53.2112 179.8898 0001365 71.7291 288.3849 15.08843155 07
| Epoch (UTC): | 25 May 2026 08:53:35 |
| Eccentricity: | 0.0001365 |
| inclination: | 53.2112° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 179.8898° |
| argument of perigee: | 71.7291° |
| revolutions per day: | 15.08843155 |
| mean anomaly at epoch: | 288.3849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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