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 66654U 26145.52521506 +.00000000 +00000-0 +15231-3 0 00009
2 66654 97.7487 75.0388 0014779 73.8684 286.4162 14.92977216 03
| Epoch (UTC): | 25 May 2026 12:36:18 |
| Eccentricity: | 0.0014779 |
| inclination: | 97.7487° |
| perigee height: | 578 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 75.0388° |
| argument of perigee: | 73.8684° |
| revolutions per day: | 14.92977216 |
| mean anomaly at epoch: | 286.4162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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