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 22143.56369361 .00000039 00000-0 56066-4 0 9991
2 00082 38.8615 107.5413 1173409 246.4374 100.8886 12.26015329894350
| Epoch (UTC): | 23 May 2022 13:31:43 |
| Eccentricity: | 0.1173409 |
| inclination: | 38.8615° |
| perigee height: | 634 km |
| apogee height: | 2498 km |
| right ascension of ascending node: | 107.5413° |
| argument of perigee: | 246.4374° |
| revolutions per day: | 12.26015329 |
| mean anomaly at epoch: | 100.8886° |
| orbit number at epoch: | 89435 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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