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 53425U 26145.37514875 +.00000000 +00000-0 +59539-3 0 00004
2 53425 53.2113 129.8646 0001171 66.0252 294.0863 15.08806296 00
| Epoch (UTC): | 25 May 2026 09:00:12 |
| Eccentricity: | 0.0001171 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 129.8646° |
| argument of perigee: | 66.0252° |
| revolutions per day: | 15.08806296 |
| mean anomaly at epoch: | 294.0863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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