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 66349U 26145.61992399 +.00000000 +00000-0 +36004-3 0 00003
2 66349 53.1587 235.1515 0000427 121.8557 238.2485 15.30206018 01
| Epoch (UTC): | 25 May 2026 14:52:41 |
| Eccentricity: | 0.0000427 |
| inclination: | 53.1587° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 235.1515° |
| argument of perigee: | 121.8557° |
| revolutions per day: | 15.30206018 |
| mean anomaly at epoch: | 238.2485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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