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 20442U 90005G 23156.16347978 .00000152 00000-0 72081-4 0 9998
2 20442 98.8431 132.4228 0011085 209.3138 150.7425 14.33258478743687
| Epoch (UTC): | 05 June 2023 03:55:24 |
| Eccentricity: | 0.0011085 |
| inclination: | 98.8431° |
| perigee height: | 773 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 132.4228° |
| argument of perigee: | 209.3138° |
| revolutions per day: | 14.33258478 |
| mean anomaly at epoch: | 150.7425° |
| orbit number at epoch: | 74368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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