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 26064.93525759 +.00000000 +00000-0 -43375-4 0 00000
2 17973 70.8996 42.0939 0029792 23.4445 336.8027 14.14552932 01
| Epoch (UTC): | 05 March 2026 22:26:46 |
| Eccentricity: | 0.0029792 |
| inclination: | 70.8996° |
| perigee height: | 822 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 42.0939° |
| argument of perigee: | 23.4445° |
| revolutions per day: | 14.14552932 |
| mean anomaly at epoch: | 336.8027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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