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 48274U 21035A 22221.56660412 .00008636 00000-0 10131-3 0 9997
2 48274 41.4734 253.8378 0005575 16.0032 120.5915 15.61615027 73119
| Epoch (UTC): | 09 August 2022 13:35:54 |
| Eccentricity: | 0.0005575 |
| inclination: | 41.4734° |
| perigee height: | 379 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 253.8378° |
| argument of perigee: | 16.0032° |
| revolutions per day: | 15.61615027 |
| mean anomaly at epoch: | 120.5915° |
| orbit number at epoch: | 7311 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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