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 39434U 13066U 23177.13531690 .10835562 24672-5 28689-2 0 9998
2 39434 97.3764 251.1059 0016836 265.5422 94.3948 16.28032842526842
| Epoch (UTC): | 26 June 2023 03:14:51 |
| Eccentricity: | 0.0016836 |
| inclination: | 97.3764° |
| perigee height: | 187 km |
| apogee height: | 209 km |
| right ascension of ascending node: | 251.1059° |
| argument of perigee: | 265.5422° |
| revolutions per day: | 16.28032842 |
| mean anomaly at epoch: | 94.3948° |
| orbit number at epoch: | 52684 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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