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 05485U 71080A 22181.56172428 .00000052 00000-0 45571-4 0 9990
2 05485 32.0539 246.4774 0640003 188.1904 170.7785 12.74148400364531
| Epoch (UTC): | 30 June 2022 13:28:52 |
| Eccentricity: | 0.0640003 |
| inclination: | 32.0539° |
| perigee height: | 869 km |
| apogee height: | 1860 km |
| right ascension of ascending node: | 246.4774° |
| argument of perigee: | 188.1904° |
| revolutions per day: | 12.74148400 |
| mean anomaly at epoch: | 170.7785° |
| orbit number at epoch: | 36453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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