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 62606U 26145.44501484 +.00000000 +00000-0 +69485-3 0 00006
2 62606 42.9981 204.3984 0001335 269.1384 90.9314 15.27593527 02
| Epoch (UTC): | 25 May 2026 10:40:49 |
| Eccentricity: | 0.0001335 |
| inclination: | 42.9981° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.3984° |
| argument of perigee: | 269.1384° |
| revolutions per day: | 15.27593527 |
| mean anomaly at epoch: | 90.9314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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