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 22148.53357536 -.00000025 00000-0 54792-5 0 9995
2 00082 38.8635 89.1459 1173488 270.3931 76.2671 12.26015681894965
| Epoch (UTC): | 28 May 2022 12:48:20 |
| Eccentricity: | 0.1173488 |
| inclination: | 38.8635° |
| perigee height: | 634 km |
| apogee height: | 2499 km |
| right ascension of ascending node: | 89.1459° |
| argument of perigee: | 270.3931° |
| revolutions per day: | 12.26015681 |
| mean anomaly at epoch: | 76.2671° |
| orbit number at epoch: | 89496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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