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 10521U 77119B 22227.68947806 .00000116 00000-0 44285-4 0 9992
2 10521 74.0285 16.9375 0021902 289.2682 70.6104 14.40939553343493
| Epoch (UTC): | 15 August 2022 16:32:50 |
| Eccentricity: | 0.0021902 |
| inclination: | 74.0285° |
| perigee height: | 740 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 16.9375° |
| argument of perigee: | 289.2682° |
| revolutions per day: | 14.40939553 |
| mean anomaly at epoch: | 70.6104° |
| orbit number at epoch: | 34349 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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