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 62597U 26145.35552635 +.00000000 +00000-0 +14429-2 0 00006
2 62597 43.0021 23.8800 0001293 290.4900 69.5829 15.70892912 04
| Epoch (UTC): | 25 May 2026 08:31:57 |
| Eccentricity: | 0.0001293 |
| inclination: | 43.0021° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 23.8800° |
| argument of perigee: | 290.4900° |
| revolutions per day: | 15.70892912 |
| mean anomaly at epoch: | 69.5829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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