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 17973U 26111.96020336 +.00000000 +00000-0 -12837-3 0 00005
2 17973 70.8986 302.9082 0032714 314.3889 45.4554 14.14562385 00
| Epoch (UTC): | 21 April 2026 23:02:41 |
| Eccentricity: | 0.0032714 |
| inclination: | 70.8986° |
| perigee height: | 820 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 302.9082° |
| argument of perigee: | 314.3889° |
| revolutions per day: | 14.14562385 |
| mean anomaly at epoch: | 45.4554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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