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 01726U 65089A 23088.92444594 -.00000083 00000-0 -51277-4 0 9995
2 01726 59.3789 150.9075 0716692 172.2442 0.2742 11.97055356508953
| Epoch (UTC): | 29 March 2023 22:11:12 |
| Eccentricity: | 0.0716692 |
| inclination: | 59.3789° |
| perigee height: | 1115 km |
| apogee height: | 2272 km |
| right ascension of ascending node: | 150.9075° |
| argument of perigee: | 172.2442° |
| revolutions per day: | 11.97055356 |
| mean anomaly at epoch: | 0.2742° |
| orbit number at epoch: | 50895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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