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 39194U 13032A 22142.07406544 .00071002 00000-0 93340-3 0 9998
2 39194 74.7022 13.3564 0006495 174.2103 185.9195 15.58155287498774
| Epoch (UTC): | 22 May 2022 01:46:39 |
| Eccentricity: | 0.0006495 |
| inclination: | 74.7022° |
| perigee height: | 388 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 13.3564° |
| argument of perigee: | 174.2103° |
| revolutions per day: | 15.58155287 |
| mean anomaly at epoch: | 185.9195° |
| orbit number at epoch: | 49877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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