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 22178.41888143 .00001451 00000-0 19256-3 0 9996
2 39446 97.6859 142.0512 0070124 57.5228 303.2738 14.79594519461933
| Epoch (UTC): | 27 June 2022 10:03:11 |
| Eccentricity: | 0.0070124 |
| inclination: | 97.6859° |
| perigee height: | 581 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 142.0512° |
| argument of perigee: | 57.5228° |
| revolutions per day: | 14.79594519 |
| mean anomaly at epoch: | 303.2738° |
| orbit number at epoch: | 46193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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