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 66153U 26145.48927456 +.00000000 +00000-0 +57166-3 0 00005
2 66153 53.1598 65.6075 0001290 87.0593 273.0557 15.34401730 04
| Epoch (UTC): | 25 May 2026 11:44:33 |
| Eccentricity: | 0.0001290 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 65.6075° |
| argument of perigee: | 87.0593° |
| revolutions per day: | 15.34401730 |
| mean anomaly at epoch: | 273.0557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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