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 26069.58650091 +.00000000 +00000-0 +11071-3 0 00003
2 20323 97.0705 276.8826 0070510 119.1983 241.6292 14.50663824 09
| Epoch (UTC): | 10 March 2026 14:04:33 |
| Eccentricity: | 0.0070510 |
| inclination: | 97.0705° |
| perigee height: | 673 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 276.8826° |
| argument of perigee: | 119.1983° |
| revolutions per day: | 14.50663824 |
| mean anomaly at epoch: | 241.6292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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