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 00045U 60007A 22147.81496531 .00000524 00000-0 15821-3 0 9996
2 00045 66.6944 311.3693 0252471 160.8880 200.1909 14.33846493167521
| Epoch (UTC): | 27 May 2022 19:33:33 |
| Eccentricity: | 0.0252471 |
| inclination: | 66.6944° |
| perigee height: | 598 km |
| apogee height: | 959 km |
| right ascension of ascending node: | 311.3693° |
| argument of perigee: | 160.8880° |
| revolutions per day: | 14.33846493 |
| mean anomaly at epoch: | 200.1909° |
| orbit number at epoch: | 16752 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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