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 11608U 26063.82039890 +.00000000 +00000-0 +38496-4 0 00009
2 11608 81.2169 1.8009 0052942 218.8398 140.8962 14.06551439 02
| Epoch (UTC): | 04 March 2026 19:41:22 |
| Eccentricity: | 0.0052942 |
| inclination: | 81.2169° |
| perigee height: | 833 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 1.8009° |
| argument of perigee: | 218.8398° |
| revolutions per day: | 14.06551439 |
| mean anomaly at epoch: | 140.8962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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