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 00082U 61004B 22175.50698474 -.00000017 00000-0 36992-4 0 9993
2 00082 38.8565 349.2930 1171674 40.5192 327.7038 12.26016249898272
| Epoch (UTC): | 24 June 2022 12:10:03 |
| Eccentricity: | 0.1171674 |
| inclination: | 38.8565° |
| perigee height: | 635 km |
| apogee height: | 2497 km |
| right ascension of ascending node: | 349.2930° |
| argument of perigee: | 40.5192° |
| revolutions per day: | 12.26016249 |
| mean anomaly at epoch: | 327.7038° |
| orbit number at epoch: | 89827 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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