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 62897U 26145.34679108 +.00000000 +00000-0 +44097-3 0 00008
2 62897 42.9981 252.1037 0001422 285.0784 74.9910 15.27583114 07
| Epoch (UTC): | 25 May 2026 08:19:22 |
| Eccentricity: | 0.0001422 |
| inclination: | 42.9981° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 252.1037° |
| argument of perigee: | 285.0784° |
| revolutions per day: | 15.27583114 |
| mean anomaly at epoch: | 74.9910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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