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 19650U 26066.50334147 +.00000000 +00000-0 +15138-3 0 00002
2 19650 71.0001 156.0975 0013805 5.0416 355.0844 14.16150712 05
| Epoch (UTC): | 07 March 2026 12:04:48 |
| Eccentricity: | 0.0013805 |
| inclination: | 71.0001° |
| perigee height: | 828 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 156.0975° |
| argument of perigee: | 5.0416° |
| revolutions per day: | 14.16150712 |
| mean anomaly at epoch: | 355.0844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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