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 53393U 26145.28224220 +.00000000 +00000-0 -93250-5 0 00001
2 53393 53.2137 140.2832 0001235 71.1716 288.9410 15.08829854 02
| Epoch (UTC): | 25 May 2026 06:46:25 |
| Eccentricity: | 0.0001235 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 140.2832° |
| argument of perigee: | 71.1716° |
| revolutions per day: | 15.08829854 |
| mean anomaly at epoch: | 288.9410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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