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 23150.90811240 -.00000231 00000-0 -95203-4 0 9996
2 23088 71.0017 39.5131 0002716 351.9548 8.1531 14.14767926502699
| Epoch (UTC): | 30 May 2023 21:47:40 |
| Eccentricity: | 0.0002716 |
| inclination: | 71.0017° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 39.5131° |
| argument of perigee: | 351.9548° |
| revolutions per day: | 14.14767926 |
| mean anomaly at epoch: | 8.1531° |
| orbit number at epoch: | 50269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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