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 66087U 26145.62059500 +.00000000 +00000-0 +62527-3 0 00000
2 66087 53.1591 106.4940 0001637 92.0209 268.0979 15.30210607 02
| Epoch (UTC): | 25 May 2026 14:53:39 |
| Eccentricity: | 0.0001637 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.4940° |
| argument of perigee: | 92.0209° |
| revolutions per day: | 15.30210607 |
| mean anomaly at epoch: | 268.0979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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