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 66054U 26145.63085250 +.00000000 +00000-0 +22493-3 0 00004
2 66054 97.4769 215.0368 0011743 164.9170 195.2418 15.20773324 08
| Epoch (UTC): | 25 May 2026 15:08:25 |
| Eccentricity: | 0.0011743 |
| inclination: | 97.4769° |
| perigee height: | 495 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 215.0368° |
| argument of perigee: | 164.9170° |
| revolutions per day: | 15.20773324 |
| mean anomaly at epoch: | 195.2418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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