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 39136U 13015G 23088.84665604 .00047922 00000-0 14224-2 0 9991
2 39136 64.8699 252.4414 0025996 280.2534 79.5669 15.34191978549483
| Epoch (UTC): | 29 March 2023 20:19:11 |
| Eccentricity: | 0.0025996 |
| inclination: | 64.8699° |
| perigee height: | 445 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 252.4414° |
| argument of perigee: | 280.2534° |
| revolutions per day: | 15.34191978 |
| mean anomaly at epoch: | 79.5669° |
| orbit number at epoch: | 54948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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