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 46609U 20061BH 22181.14367288 .00006806 00000-0 31033-3 0 9990
2 46609 97.3917 252.0135 0004715 83.4096 276.7676 15.20948747 95325
| Epoch (UTC): | 30 June 2022 03:26:53 |
| Eccentricity: | 0.0004715 |
| inclination: | 97.3917° |
| perigee height: | 500 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 252.0135° |
| argument of perigee: | 83.4096° |
| revolutions per day: | 15.20948747 |
| mean anomaly at epoch: | 276.7676° |
| orbit number at epoch: | 9532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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