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 66273U 26145.39775588 +.00000000 +00000-0 +72992-3 0 00009
2 66273 53.1599 194.0371 0000886 38.7552 321.3514 15.34403458 01
| Epoch (UTC): | 25 May 2026 09:32:46 |
| Eccentricity: | 0.0000886 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 194.0371° |
| argument of perigee: | 38.7552° |
| revolutions per day: | 15.34403458 |
| mean anomaly at epoch: | 321.3514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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