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 26019.10718942 +.00000000 +00000-0 +13247-3 0 00004
2 19650 70.9985 255.8208 0011947 85.7523 274.4966 14.16146173 05
| Epoch (UTC): | 19 January 2026 02:34:21 |
| Eccentricity: | 0.0011947 |
| inclination: | 70.9985° |
| perigee height: | 830 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 255.8208° |
| argument of perigee: | 85.7523° |
| revolutions per day: | 14.16146173 |
| mean anomaly at epoch: | 274.4966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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