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 26044.64244800 +.00000000 +00000-0 +12800-3 0 00004
2 11416 98.5783 74.9384 0008709 263.4713 96.5481 14.35414858 06
| Epoch (UTC): | 13 February 2026 15:25:07 |
| Eccentricity: | 0.0008709 |
| inclination: | 98.5783° |
| perigee height: | 767 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 74.9384° |
| argument of perigee: | 263.4713° |
| revolutions per day: | 14.35414858 |
| mean anomaly at epoch: | 96.5481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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