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 66169U 26145.48033549 +.00000000 +00000-0 +63008-3 0 00005
2 66169 53.1583 66.2424 0001167 93.4172 266.6962 15.30206672 09
| Epoch (UTC): | 25 May 2026 11:31:40 |
| Eccentricity: | 0.0001167 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 66.2424° |
| argument of perigee: | 93.4172° |
| revolutions per day: | 15.30206672 |
| mean anomaly at epoch: | 266.6962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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