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 23432U 94083B 22225.08923035 .00000058 00000-0 30413-4 0 9999
2 23432 74.0314 94.4715 0005950 215.5792 296.9111 14.33620622445882
| Epoch (UTC): | 13 August 2022 02:08:29 |
| Eccentricity: | 0.0005950 |
| inclination: | 74.0314° |
| perigee height: | 775 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 94.4715° |
| argument of perigee: | 215.5792° |
| revolutions per day: | 14.33620622 |
| mean anomaly at epoch: | 296.9111° |
| orbit number at epoch: | 44588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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