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 26088.18822339 +.00000000 +00000-0 -24587-4 0 00005
2 19650 70.9970 110.4700 0015143 332.4864 27.5456 14.16153561 04
| Epoch (UTC): | 29 March 2026 04:31:02 |
| Eccentricity: | 0.0015143 |
| inclination: | 70.9970° |
| perigee height: | 827 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 110.4700° |
| argument of perigee: | 332.4864° |
| revolutions per day: | 14.16153561 |
| mean anomaly at epoch: | 27.5456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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