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 06080U 26064.56156501 +.00000000 +00000-0 +57005-4 0 00005
2 06080 81.2420 172.3751 0048576 355.5521 4.5206 14.01289586 06
| Epoch (UTC): | 05 March 2026 13:28:39 |
| Eccentricity: | 0.0048576 |
| inclination: | 81.2420° |
| perigee height: | 854 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 172.3751° |
| argument of perigee: | 355.5521° |
| revolutions per day: | 14.01289586 |
| mean anomaly at epoch: | 4.5206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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