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 23150.13036803 -.00000221 00000-0 -90031-4 0 9998
2 23088 71.0018 41.1457 0002678 352.9913 7.1171 14.14768158502859
| Epoch (UTC): | 30 May 2023 03:07:43 |
| Eccentricity: | 0.0002678 |
| inclination: | 71.0018° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 41.1457° |
| argument of perigee: | 352.9913° |
| revolutions per day: | 14.14768158 |
| mean anomaly at epoch: | 7.1171° |
| orbit number at epoch: | 50285 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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