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 53413U 26145.27946626 +.00000000 +00000-0 +36940-4 0 00005
2 53413 53.2132 130.2954 0001182 95.3201 264.7926 15.08842060 00
| Epoch (UTC): | 25 May 2026 06:42:25 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 130.2954° |
| argument of perigee: | 95.3201° |
| revolutions per day: | 15.08842060 |
| mean anomaly at epoch: | 264.7926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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