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 22268.28313216 .00006440 00000-0 64107-3 0 9993
2 39770 97.9485 25.9528 0009537 115.0217 245.2019 14.91951900452544
| Epoch (UTC): | 25 September 2022 06:47:42 |
| Eccentricity: | 0.0009537 |
| inclination: | 97.9485° |
| perigee height: | 585 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 25.9528° |
| argument of perigee: | 115.0217° |
| revolutions per day: | 14.91951900 |
| mean anomaly at epoch: | 245.2019° |
| orbit number at epoch: | 45254 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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