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 23157.05936997 -.00000231 00000-0 -95191-4 0 9992
2 23088 71.0006 26.6000 0002996 346.3047 13.7994 14.14765622503834
| Epoch (UTC): | 06 June 2023 01:25:29 |
| Eccentricity: | 0.0002996 |
| inclination: | 71.0006° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 26.6000° |
| argument of perigee: | 346.3047° |
| revolutions per day: | 14.14765622 |
| mean anomaly at epoch: | 13.7994° |
| orbit number at epoch: | 50383 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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