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 16720U 26064.20205300 +.00000000 +00000-0 +66004-4 0 00009
2 16720 82.5560 151.2303 0020036 35.2430 353.4194 14.85663557 06
| Epoch (UTC): | 05 March 2026 04:50:57 |
| Eccentricity: | 0.0020036 |
| inclination: | 82.5560° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 151.2303° |
| argument of perigee: | 35.2430° |
| revolutions per day: | 14.85663557 |
| mean anomaly at epoch: | 353.4194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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