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 66562U 26145.08640444 +.00000000 +00000-0 +64970-3 0 00005
2 66562 43.0019 275.6163 0003602 266.3709 93.6731 15.27590801 05
| Epoch (UTC): | 25 May 2026 02:04:25 |
| Eccentricity: | 0.0003602 |
| inclination: | 43.0019° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 275.6163° |
| argument of perigee: | 266.3709° |
| revolutions per day: | 15.27590801 |
| mean anomaly at epoch: | 93.6731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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