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 22146.79118669 .00000117 00000-0 40250-4 0 9990
2 00059 28.2457 179.5835 0189293 111.5143 250.5693 13.53000163 42244
| Epoch (UTC): | 26 May 2022 18:59:18 |
| Eccentricity: | 0.0189293 |
| inclination: | 28.2457° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 179.5835° |
| argument of perigee: | 111.5143° |
| revolutions per day: | 13.53000163 |
| mean anomaly at epoch: | 250.5693° |
| orbit number at epoch: | 4224 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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