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 37386U 11014A 22221.05062960 0.00000000 00000-0 00000-0 0 04
2 37386 63.4447 273.1692 0245006 357.6304 2.3696 13.40842532 00
| Epoch (UTC): | 09 August 2022 01:12:54 |
| Eccentricity: | 0.0245006 |
| inclination: | 63.4447° |
| perigee height: | 923 km |
| apogee height: | 1289 km |
| right ascension of ascending node: | 273.1692° |
| argument of perigee: | 357.6304° |
| revolutions per day: | 13.40842532 |
| mean anomaly at epoch: | 2.3696° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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