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 23088U 94023B 24281.80877889 .00000139 00000-0 96735-4 0 9998
2 23088 70.9995 78.3979 0004117 327.2019 32.8847 14.14894542573102
| Epoch (UTC): | 07 October 2024 19:24:38 |
| Eccentricity: | 0.0004117 |
| inclination: | 70.9995° |
| perigee height: | 840 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 78.3979° |
| argument of perigee: | 327.2019° |
| revolutions per day: | 14.14894542 |
| mean anomaly at epoch: | 32.8847° |
| orbit number at epoch: | 57310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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