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 23272.24155321 .00007030 00000-0 29936-3 0 9993
2 39679 51.6101 284.4708 0149357 154.4739 206.3707 15.14567082520321
| Epoch (UTC): | 29 September 2023 05:47:50 |
| Eccentricity: | 0.0149357 |
| inclination: | 51.6101° |
| perigee height: | 419 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 284.4708° |
| argument of perigee: | 154.4739° |
| revolutions per day: | 15.14567082 |
| mean anomaly at epoch: | 206.3707° |
| orbit number at epoch: | 52032 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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