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 22178.89227171 .00001256 00000-0 16753-3 0 9998
2 39446 97.6859 142.5041 0070097 56.0128 304.7718 14.79594836462002
| Epoch (UTC): | 27 June 2022 21:24:52 |
| Eccentricity: | 0.0070097 |
| inclination: | 97.6859° |
| perigee height: | 581 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 142.5041° |
| argument of perigee: | 56.0128° |
| revolutions per day: | 14.79594836 |
| mean anomaly at epoch: | 304.7718° |
| orbit number at epoch: | 46200 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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