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 52125U 26145.52832920 +.00000000 +00000-0 -48820-4 0 00004
2 52125 53.2125 84.1776 0001251 94.6882 265.4253 15.08839202 09
| Epoch (UTC): | 25 May 2026 12:40:47 |
| Eccentricity: | 0.0001251 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.1776° |
| argument of perigee: | 94.6882° |
| revolutions per day: | 15.08839202 |
| mean anomaly at epoch: | 265.4253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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