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 39679U 14021B 22144.19438394 .00003474 00000-0 17688-3 0 9997
2 39679 51.6156 68.9215 0164763 233.8371 124.7262 15.08571235445458
| Epoch (UTC): | 24 May 2022 04:39:54 |
| Eccentricity: | 0.0164763 |
| inclination: | 51.6156° |
| perigee height: | 426 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 68.9215° |
| argument of perigee: | 233.8371° |
| revolutions per day: | 15.08571235 |
| mean anomaly at epoch: | 124.7262° |
| orbit number at epoch: | 44545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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