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 52282U 26145.29005262 +.00000000 +00000-0 +46895-4 0 00002
2 52282 53.2134 115.2434 0001705 70.2712 289.8464 15.08836280 03
| Epoch (UTC): | 25 May 2026 06:57:40 |
| Eccentricity: | 0.0001705 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.2434° |
| argument of perigee: | 70.2712° |
| revolutions per day: | 15.08836280 |
| mean anomaly at epoch: | 289.8464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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