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 52105U 26145.27075852 +.00000000 +00000-0 +13863-3 0 00004
2 52105 53.2134 95.3349 0001515 32.6699 327.4387 15.08856204 06
| Epoch (UTC): | 25 May 2026 06:29:53 |
| Eccentricity: | 0.0001515 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.3349° |
| argument of perigee: | 32.6699° |
| revolutions per day: | 15.08856204 |
| mean anomaly at epoch: | 327.4387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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