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 25544U 98067A 22221.01449514 -.00010455 00000-0 -17350-3 0 9993
2 25544 51.6440 74.8941 0004893 93.8437 53.3817 15.50294862353373
| Epoch (UTC): | 09 August 2022 00:20:52 |
| Eccentricity: | 0.0004893 |
| inclination: | 51.6440° |
| perigee height: | 412 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 74.8941° |
| argument of perigee: | 93.8437° |
| revolutions per day: | 15.50294862 |
| mean anomaly at epoch: | 53.3817° |
| orbit number at epoch: | 35337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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