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 26103.74146329 +.00000000 +00000-0 +83978-4 0 00007
2 06173 90.0215 208.5780 0047287 255.5631 267.1365 14.52588961 00
| Epoch (UTC): | 13 April 2026 17:47:42 |
| Eccentricity: | 0.0047287 |
| inclination: | 90.0215° |
| perigee height: | 684 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 208.5780° |
| argument of perigee: | 255.5631° |
| revolutions per day: | 14.52588961 |
| mean anomaly at epoch: | 267.1365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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