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 66616U 26145.58811543 +.00000000 +00000-0 +67271-3 0 00007
2 66616 42.9986 342.1384 0000909 271.8268 88.2480 15.27581840 03
| Epoch (UTC): | 25 May 2026 14:06:53 |
| Eccentricity: | 0.0000909 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.1384° |
| argument of perigee: | 271.8268° |
| revolutions per day: | 15.27581840 |
| mean anomaly at epoch: | 88.2480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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