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 66166U 26145.19084999 +.00000000 +00000-0 +72788-3 0 00000
2 66166 53.1602 66.5717 0001112 74.9757 285.1368 15.34368136 03
| Epoch (UTC): | 25 May 2026 04:34:49 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 66.5717° |
| argument of perigee: | 74.9757° |
| revolutions per day: | 15.34368136 |
| mean anomaly at epoch: | 285.1368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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