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 11416U 26040.04182894 +.00000000 +00000-0 +13357-3 0 00006
2 11416 98.5788 70.3644 0008711 278.9102 81.1097 14.35411141 01
| Epoch (UTC): | 09 February 2026 01:00:14 |
| Eccentricity: | 0.0008711 |
| inclination: | 98.5788° |
| perigee height: | 767 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 70.3644° |
| argument of perigee: | 278.9102° |
| revolutions per day: | 14.35411141 |
| mean anomaly at epoch: | 81.1097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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