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 22331.61544419 .00000115 00000-0 30758-4 0 9993
2 00059 28.2505 310.1438 0189141 222.8324 135.7345 13.53009927 67296
| Epoch (UTC): | 27 November 2022 14:46:14 |
| Eccentricity: | 0.0189141 |
| inclination: | 28.2505° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 310.1438° |
| argument of perigee: | 222.8324° |
| revolutions per day: | 13.53009927 |
| mean anomaly at epoch: | 135.7345° |
| orbit number at epoch: | 6729 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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