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 52119U 26145.55685241 +.00000000 +00000-0 +99541-4 0 00007
2 52119 53.2133 94.0496 0001313 79.0465 281.0675 15.08829476 07
| Epoch (UTC): | 25 May 2026 13:21:52 |
| Eccentricity: | 0.0001313 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 94.0496° |
| argument of perigee: | 79.0465° |
| revolutions per day: | 15.08829476 |
| mean anomaly at epoch: | 281.0675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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