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 23155.90261873 .00017873 00000-0 13728-2 0 9993
2 39770 97.9850 282.7749 0006121 343.2968 16.8053 15.01799248490316
| Epoch (UTC): | 04 June 2023 21:39:46 |
| Eccentricity: | 0.0006121 |
| inclination: | 97.9850° |
| perigee height: | 557 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 282.7749° |
| argument of perigee: | 343.2968° |
| revolutions per day: | 15.01799248 |
| mean anomaly at epoch: | 16.8053° |
| orbit number at epoch: | 49031 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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