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 62594U 26145.58335647 +.00000000 +00000-0 +36535-3 0 00003
2 62594 42.9918 19.3895 0010010 245.4992 112.2129 15.82297421 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0010010 |
| inclination: | 42.9918° |
| perigee height: | 317 km |
| apogee height: | 331 km |
| right ascension of ascending node: | 19.3895° |
| argument of perigee: | 245.4992° |
| revolutions per day: | 15.82297421 |
| mean anomaly at epoch: | 112.2129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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