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 66242U 26145.11867869 +.00000000 +00000-0 +39898-3 0 00007
2 66242 53.1602 289.2072 0001601 87.6497 272.4687 15.30205521 08
| Epoch (UTC): | 25 May 2026 02:50:53 |
| Eccentricity: | 0.0001601 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 289.2072° |
| argument of perigee: | 87.6497° |
| revolutions per day: | 15.30205521 |
| mean anomaly at epoch: | 272.4687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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