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 26071.37459309 +.00000000 +00000-0 +14488-3 0 00005
2 17974 71.0097 27.1659 0014886 209.2683 322.6413 14.17642830 08
| Epoch (UTC): | 12 March 2026 08:59:24 |
| Eccentricity: | 0.0014886 |
| inclination: | 71.0097° |
| perigee height: | 823 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 27.1659° |
| argument of perigee: | 209.2683° |
| revolutions per day: | 14.17642830 |
| mean anomaly at epoch: | 322.6413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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