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 26620U 26150.49782994 +.00000000 +00000-0 +14288-3 0 00001
2 26620 98.4970 161.8278 0001632 87.9657 272.1731 14.62906355 06
| Epoch (UTC): | 30 May 2026 11:56:52 |
| Eccentricity: | 0.0001632 |
| inclination: | 98.4970° |
| perigee height: | 683 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 161.8278° |
| argument of perigee: | 87.9657° |
| revolutions per day: | 14.62906355 |
| mean anomaly at epoch: | 272.1731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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