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 23155.92810332 -.00000243 00000-0 -10145-3 0 9998
2 23088 71.0008 28.9750 0002933 347.2140 12.8907 14.14766049503409
| Epoch (UTC): | 04 June 2023 22:16:28 |
| Eccentricity: | 0.0002933 |
| inclination: | 71.0008° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 28.9750° |
| argument of perigee: | 347.2140° |
| revolutions per day: | 14.14766049 |
| mean anomaly at epoch: | 12.8907° |
| orbit number at epoch: | 50340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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