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 62518U 26145.53406543 +.00000000 +00000-0 +20099-2 0 00005
2 62518 43.0006 327.5807 0002470 264.1554 95.9032 15.70907164 07
| Epoch (UTC): | 25 May 2026 12:49:03 |
| Eccentricity: | 0.0002470 |
| inclination: | 43.0006° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 327.5807° |
| argument of perigee: | 264.1554° |
| revolutions per day: | 15.70907164 |
| mean anomaly at epoch: | 95.9032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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