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 66942U 26145.50003470 +.00000000 +00000-0 +21195-1 0 00006
2 66942 53.1604 1.4486 0002606 30.4666 195.3572 15.33582660 01
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0002606 |
| inclination: | 53.1604° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 1.4486° |
| argument of perigee: | 30.4666° |
| revolutions per day: | 15.33582660 |
| mean anomaly at epoch: | 195.3572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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