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 66832U 26145.39242345 +.00000000 +00000-0 +14903-3 0 00008
2 66832 70.0006 141.1262 0003641 261.0033 99.0714 14.98337383 05
| Epoch (UTC): | 25 May 2026 09:25:05 |
| Eccentricity: | 0.0003641 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.1262° |
| argument of perigee: | 261.0033° |
| revolutions per day: | 14.98337383 |
| mean anomaly at epoch: | 99.0714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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