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 39444U 13066AE 22178.63678885 .00001620 00000-0 19795-3 0 9994
2 39444 97.6240 152.0802 0056678 1.2661 358.8687 14.83469983463621
| Epoch (UTC): | 27 June 2022 15:16:58 |
| Eccentricity: | 0.0056678 |
| inclination: | 97.6240° |
| perigee height: | 579 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 152.0802° |
| argument of perigee: | 1.2661° |
| revolutions per day: | 14.83469983 |
| mean anomaly at epoch: | 358.8687° |
| orbit number at epoch: | 46362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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