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 62418U 26145.49183139 +.00000000 +00000-0 +18917-2 0 00008
2 62418 43.0008 64.3533 0000477 336.6752 23.4094 15.70900550 06
| Epoch (UTC): | 25 May 2026 11:48:14 |
| Eccentricity: | 0.0000477 |
| inclination: | 43.0008° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 64.3533° |
| argument of perigee: | 336.6752° |
| revolutions per day: | 15.70900550 |
| mean anomaly at epoch: | 23.4094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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