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 66657U 26145.54249334 +.00000000 +00000-0 +20482-3 0 00004
2 66657 97.7481 75.1595 0013780 89.6442 270.6356 14.93435136 00
| Epoch (UTC): | 25 May 2026 13:01:11 |
| Eccentricity: | 0.0013780 |
| inclination: | 97.7481° |
| perigee height: | 578 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 75.1595° |
| argument of perigee: | 89.6442° |
| revolutions per day: | 14.93435136 |
| mean anomaly at epoch: | 270.6356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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