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 26067.63350137 +.00000000 +00000-0 +17681-3 0 00009
2 19650 71.0000 153.7196 0013889 3.3231 356.7981 14.16151420 08
| Epoch (UTC): | 08 March 2026 15:12:14 |
| Eccentricity: | 0.0013889 |
| inclination: | 71.0000° |
| perigee height: | 828 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 153.7196° |
| argument of perigee: | 3.3231° |
| revolutions per day: | 14.16151420 |
| mean anomaly at epoch: | 356.7981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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