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 00059U 60013B 22220.20451865 .00000106 00000-0 27207-4 0 9992
2 00059 28.2473 162.4630 0189054 7.7733 352.5684 13.53002768 52193
| Epoch (UTC): | 08 August 2022 04:54:30 |
| Eccentricity: | 0.0189054 |
| inclination: | 28.2473° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 162.4630° |
| argument of perigee: | 7.7733° |
| revolutions per day: | 13.53002768 |
| mean anomaly at epoch: | 352.5684° |
| orbit number at epoch: | 5219 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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