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 61252U 26145.41488698 +.00000000 +00000-0 +51089-5 0 00003
2 61252 53.1584 38.2842 0000744 78.5620 281.5482 15.69706467 05
| Epoch (UTC): | 25 May 2026 09:57:26 |
| Eccentricity: | 0.0000744 |
| inclination: | 53.1584° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 38.2842° |
| argument of perigee: | 78.5620° |
| revolutions per day: | 15.69706467 |
| mean anomaly at epoch: | 281.5482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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