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 26073.57035451 +.00000000 +00000-0 +13778-3 0 00003
2 11416 98.5745 103.6944 0010024 172.3502 187.7838 14.35437713 07
| Epoch (UTC): | 14 March 2026 13:41:18 |
| Eccentricity: | 0.0010024 |
| inclination: | 98.5745° |
| perigee height: | 766 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 103.6944° |
| argument of perigee: | 172.3502° |
| revolutions per day: | 14.35437713 |
| mean anomaly at epoch: | 187.7838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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