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 26042.06331428 +.00000000 +00000-0 +13283-3 0 00007
2 11416 98.5786 72.3742 0008716 272.1159 87.9028 14.35412870 01
| Epoch (UTC): | 11 February 2026 01:31:10 |
| Eccentricity: | 0.0008716 |
| inclination: | 98.5786° |
| perigee height: | 767 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 72.3742° |
| argument of perigee: | 272.1159° |
| revolutions per day: | 14.35412870 |
| mean anomaly at epoch: | 87.9028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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