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 17974U 26088.16374722 +.00000000 +00000-0 +77389-4 0 00005
2 17974 71.0105 351.7719 0013925 184.5592 325.4785 14.17644560 03
| Epoch (UTC): | 29 March 2026 03:55:47 |
| Eccentricity: | 0.0013925 |
| inclination: | 71.0105° |
| perigee height: | 823 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 351.7719° |
| argument of perigee: | 184.5592° |
| revolutions per day: | 14.17644560 |
| mean anomaly at epoch: | 325.4785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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