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 17160U 26021.38064339 +.00000000 +00000-0 +33279-4 0 00003
2 17160 82.9257 254.4425 0039690 37.6003 135.4555 13.74912168 02
| Epoch (UTC): | 21 January 2026 09:08:07 |
| Eccentricity: | 0.0039690 |
| inclination: | 82.9257° |
| perigee height: | 953 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 254.4425° |
| argument of perigee: | 37.6003° |
| revolutions per day: | 13.74912168 |
| mean anomaly at epoch: | 135.4555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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