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 19649U 26162.29027819 +.00000000 +00000-0 +70164-4 0 00009
2 19649 71.0003 17.4602 0005525 345.5717 14.5247 14.15214207 01
| Epoch (UTC): | 11 June 2026 06:58:00 |
| Eccentricity: | 0.0005525 |
| inclination: | 71.0003° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 17.4602° |
| argument of perigee: | 345.5717° |
| revolutions per day: | 14.15214207 |
| mean anomaly at epoch: | 14.5247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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