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 18958U 88020A 22222.04241237 .00001716 00000-0 11964-3 0 9991
2 18958 82.5275 88.5561 0011765 10.4690 349.6779 15.04764163874039
| Epoch (UTC): | 10 August 2022 01:01:04 |
| Eccentricity: | 0.0011765 |
| inclination: | 82.5275° |
| perigee height: | 544 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 88.5561° |
| argument of perigee: | 10.4690° |
| revolutions per day: | 15.04764163 |
| mean anomaly at epoch: | 349.6779° |
| orbit number at epoch: | 87403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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