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 66060U 26145.27919089 +.00000000 +00000-0 +78700-3 0 00009
2 66060 53.1620 249.8059 0001560 93.4487 266.6692 15.30240398 03
| Epoch (UTC): | 25 May 2026 06:42:02 |
| Eccentricity: | 0.0001560 |
| inclination: | 53.1620° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 249.8059° |
| argument of perigee: | 93.4487° |
| revolutions per day: | 15.30240398 |
| mean anomaly at epoch: | 266.6692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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