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 66168U 26145.20324024 +.00000000 +00000-0 +84701-3 0 00008
2 66168 53.1577 67.3567 0000975 105.1707 254.9402 15.30177323 01
| Epoch (UTC): | 25 May 2026 04:52:39 |
| Eccentricity: | 0.0000975 |
| inclination: | 53.1577° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 67.3567° |
| argument of perigee: | 105.1707° |
| revolutions per day: | 15.30177323 |
| mean anomaly at epoch: | 254.9402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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