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 22020.61858350 .00015702 00000-0 18551-3 0 9996
2 48274 41.4704 38.0536 0002509 118.2190 38.8901 15.60961657 41695
| Epoch (UTC): | 20 January 2022 14:50:45 |
| Eccentricity: | 0.0002509 |
| inclination: | 41.4704° |
| perigee height: | 383 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 38.0536° |
| argument of perigee: | 118.2190° |
| revolutions per day: | 15.60961657 |
| mean anomaly at epoch: | 38.8901° |
| orbit number at epoch: | 4169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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