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 66684U 26145.19046650 +.00000000 +00000-0 +16769-3 0 00004
2 66684 97.4275 219.2039 0007038 79.3961 280.8066 15.18993563 05
| Epoch (UTC): | 25 May 2026 04:34:16 |
| Eccentricity: | 0.0007038 |
| inclination: | 97.4275° |
| perigee height: | 504 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 219.2039° |
| argument of perigee: | 79.3961° |
| revolutions per day: | 15.18993563 |
| mean anomaly at epoch: | 280.8066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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