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 52112U 26145.66668980 +.00000000 +00000-0 +34083-2 0 00001
2 52112 53.2170 86.7140 0001090 91.1964 234.4293 15.38570637 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.2170° |
| perigee height: | 450 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 86.7140° |
| argument of perigee: | 91.1964° |
| revolutions per day: | 15.38570637 |
| mean anomaly at epoch: | 234.4293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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