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 53395U 26145.27582578 +.00000000 +00000-0 +43130-4 0 00005
2 53395 53.2131 140.3218 0001193 71.2900 288.8222 15.08831635 06
| Epoch (UTC): | 25 May 2026 06:37:11 |
| Eccentricity: | 0.0001193 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 140.3218° |
| argument of perigee: | 71.2900° |
| revolutions per day: | 15.08831635 |
| mean anomaly at epoch: | 288.8222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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