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 62413U 26145.49714679 +.00000000 +00000-0 +16520-2 0 00000
2 62413 43.0005 64.3982 0001183 69.2432 290.8562 15.70876316 07
| Epoch (UTC): | 25 May 2026 11:55:53 |
| Eccentricity: | 0.0001183 |
| inclination: | 43.0005° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 64.3982° |
| argument of perigee: | 69.2432° |
| revolutions per day: | 15.70876316 |
| mean anomaly at epoch: | 290.8562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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