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 66702U 26145.14722919 +.00000000 +00000-0 +36717-3 0 00004
2 66702 97.4197 219.0841 0005384 102.5719 257.6118 15.19841799 04
| Epoch (UTC): | 25 May 2026 03:32:00 |
| Eccentricity: | 0.0005384 |
| inclination: | 97.4197° |
| perigee height: | 503 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 219.0841° |
| argument of perigee: | 102.5719° |
| revolutions per day: | 15.19841799 |
| mean anomaly at epoch: | 257.6118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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