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 66178U 26145.57414176 +.00000000 +00000-0 +44808-3 0 00001
2 66178 53.1582 248.2373 0001473 291.8984 68.1860 15.30186190 02
| Epoch (UTC): | 25 May 2026 13:46:45 |
| Eccentricity: | 0.0001473 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.2373° |
| argument of perigee: | 291.8984° |
| revolutions per day: | 15.30186190 |
| mean anomaly at epoch: | 68.1860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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