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 18985U 88023A 22226.22726582 .00000058 00000-0 42445-4 0 9996
2 18985 82.9559 115.1398 0042643 93.4993 267.1043 13.76486440602986
| Epoch (UTC): | 14 August 2022 05:27:15 |
| Eccentricity: | 0.0042643 |
| inclination: | 82.9559° |
| perigee height: | 945 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 115.1398° |
| argument of perigee: | 93.4993° |
| revolutions per day: | 13.76486440 |
| mean anomaly at epoch: | 267.1043° |
| orbit number at epoch: | 60298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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