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 23152.11008139 -.00000235 00000-0 -97227-4 0 9998
2 23088 71.0015 36.9899 0002768 350.8757 9.2315 14.14767550502860
| Epoch (UTC): | 01 June 2023 02:38:31 |
| Eccentricity: | 0.0002768 |
| inclination: | 71.0015° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 36.9899° |
| argument of perigee: | 350.8757° |
| revolutions per day: | 14.14767550 |
| mean anomaly at epoch: | 9.2315° |
| orbit number at epoch: | 50286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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