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 66142U 26145.52484509 +.00000000 +00000-0 +00000-0 0 00007
2 66142 5.5189 299.6525 0004341 142.3557 52.4669 1.00269094 09
| Epoch (UTC): | 25 May 2026 12:35:46 |
| Eccentricity: | 0.0004341 |
| inclination: | 5.5189° |
| perigee height: | 35769 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 299.6525° |
| argument of perigee: | 142.3557° |
| revolutions per day: | 1.00269094 |
| mean anomaly at epoch: | 52.4669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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