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 23545U 95017A 23264.92466134 .00006172 00000-0 89499-3 0 9991
2 23545 69.9690 197.0098 0006867 224.7430 135.3164 14.76482868518509
| Epoch (UTC): | 21 September 2023 22:11:30 |
| Eccentricity: | 0.0006867 |
| inclination: | 69.9690° |
| perigee height: | 635 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 197.0098° |
| argument of perigee: | 224.7430° |
| revolutions per day: | 14.76482868 |
| mean anomaly at epoch: | 135.3164° |
| orbit number at epoch: | 51850 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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