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 66783U 26145.13877446 +.00000000 +00000-0 +29784-3 0 00004
2 66783 97.5250 216.5660 0014510 200.6220 159.4420 14.98739682 01
| Epoch (UTC): | 25 May 2026 03:19:50 |
| Eccentricity: | 0.0014510 |
| inclination: | 97.5250° |
| perigee height: | 561 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 216.5660° |
| argument of perigee: | 200.6220° |
| revolutions per day: | 14.98739682 |
| mean anomaly at epoch: | 159.4420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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