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 00876U 64053A 22228.44478678 .00000105 00000-0 41377-4 0 9995
2 00876 65.0612 138.7030 0121010 92.0624 269.4340 14.63934647 83504
| Epoch (UTC): | 16 August 2022 10:40:29 |
| Eccentricity: | 0.0121010 |
| inclination: | 65.0612° |
| perigee height: | 595 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 138.7030° |
| argument of perigee: | 92.0624° |
| revolutions per day: | 14.63934647 |
| mean anomaly at epoch: | 269.4340° |
| orbit number at epoch: | 8350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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