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 39770U 14029E 22177.30810478 .00005789 00000-0 59072-3 0 9997
2 39770 97.9435 294.3004 0009868 63.7717 296.4427 14.90996084438985
| Epoch (UTC): | 26 June 2022 07:23:40 |
| Eccentricity: | 0.0009868 |
| inclination: | 97.9435° |
| perigee height: | 588 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 294.3004° |
| argument of perigee: | 63.7717° |
| revolutions per day: | 14.90996084 |
| mean anomaly at epoch: | 296.4427° |
| orbit number at epoch: | 43898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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