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 52301U 26145.31580375 +.00000000 +00000-0 +63570-4 0 00009
2 52301 53.2146 115.1314 0001271 63.8127 296.2995 15.08841613 07
| Epoch (UTC): | 25 May 2026 07:34:45 |
| Eccentricity: | 0.0001271 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.1314° |
| argument of perigee: | 63.8127° |
| revolutions per day: | 15.08841613 |
| mean anomaly at epoch: | 296.2995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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