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 data is extracted from the following two-line orbital elements,
1 23705U 95058B 22140.91365901 -.00000213 00000-0 -84956-4 0 9991
2 23705 71.0225 215.0704 0010232 72.8753 287.3489 14.15172915371654
| Epoch (UTC): | 20 May 2022 21:55:40 |
| Eccentricity: | 0.0010232 |
| inclination: | 71.0225° |
| perigee height: | 834 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 215.0704° |
| argument of perigee: | 72.8753° |
| revolutions per day: | 14.15172915 |
| mean anomaly at epoch: | 287.3489° |
| orbit number at epoch: | 37165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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