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 53424U 26145.36410891 +.00000000 +00000-0 +26892-5 0 00003
2 53424 53.2130 129.9169 0001526 79.6896 280.4268 15.08843432 08
| Epoch (UTC): | 25 May 2026 08:44:19 |
| Eccentricity: | 0.0001526 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 129.9169° |
| argument of perigee: | 79.6896° |
| revolutions per day: | 15.08843432 |
| mean anomaly at epoch: | 280.4268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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