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 66742U 26145.14971130 +.00000000 +00000-0 +21713-3 0 00009
2 66742 97.4197 219.0854 0003670 71.6124 288.5510 15.19399686 06
| Epoch (UTC): | 25 May 2026 03:35:35 |
| Eccentricity: | 0.0003670 |
| inclination: | 97.4197° |
| perigee height: | 505 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 219.0854° |
| argument of perigee: | 71.6124° |
| revolutions per day: | 15.19399686 |
| mean anomaly at epoch: | 288.5510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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