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 06173U 26159.17598119 +.00000000 +00000-0 +13375-3 0 00006
2 06173 90.0204 208.7307 0051957 67.6973 355.2855 14.52647001 09
| Epoch (UTC): | 08 June 2026 04:13:24 |
| Eccentricity: | 0.0051957 |
| inclination: | 90.0204° |
| perigee height: | 680 km |
| apogee height: | 754 km |
| right ascension of ascending node: | 208.7307° |
| argument of perigee: | 67.6973° |
| revolutions per day: | 14.52647001 |
| mean anomaly at epoch: | 355.2855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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