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 26063.96047946 +.00000000 +00000-0 +64344-4 0 00001
2 19650 71.0000 161.4472 0013656 8.8749 351.2613 14.16149624 02
| Epoch (UTC): | 04 March 2026 23:03:05 |
| Eccentricity: | 0.0013656 |
| inclination: | 71.0000° |
| perigee height: | 829 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 161.4472° |
| argument of perigee: | 8.8749° |
| revolutions per day: | 14.16149624 |
| mean anomaly at epoch: | 351.2613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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