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 62497U 26145.25389933 +.00000000 +00000-0 +11316-2 0 00005
2 62497 43.0021 216.3533 0001730 275.5044 84.5610 15.27567055 08
| Epoch (UTC): | 25 May 2026 06:05:36 |
| Eccentricity: | 0.0001730 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 216.3533° |
| argument of perigee: | 275.5044° |
| revolutions per day: | 15.27567055 |
| mean anomaly at epoch: | 84.5610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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