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 20323U 26075.17353904 +.00000000 +00000-0 +10199-3 0 00008
2 20323 97.0701 281.5808 0070684 101.8684 259.0452 14.50668834 03
| Epoch (UTC): | 16 March 2026 04:09:53 |
| Eccentricity: | 0.0070684 |
| inclination: | 97.0701° |
| perigee height: | 673 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 281.5808° |
| argument of perigee: | 101.8684° |
| revolutions per day: | 14.50668834 |
| mean anomaly at epoch: | 259.0452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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