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 39446U 13066AG 22179.43328838 .00001193 00000-0 15948-3 0 9996
2 39446 97.6860 143.0218 0070071 54.2879 306.4826 14.79596090462082
| Epoch (UTC): | 28 June 2022 10:23:56 |
| Eccentricity: | 0.0070071 |
| inclination: | 97.6860° |
| perigee height: | 581 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 143.0218° |
| argument of perigee: | 54.2879° |
| revolutions per day: | 14.79596090 |
| mean anomaly at epoch: | 306.4826° |
| orbit number at epoch: | 46208 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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