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 52270U 26145.25969770 +.00000000 +00000-0 +54404-3 0 00002
2 52270 53.2134 125.4135 0001411 74.3167 285.7980 15.08797786 09
| Epoch (UTC): | 25 May 2026 06:13:57 |
| Eccentricity: | 0.0001411 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 125.4135° |
| argument of perigee: | 74.3167° |
| revolutions per day: | 15.08797786 |
| mean anomaly at epoch: | 285.7980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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