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 42200U 81053TQ 23333.79019902 .00004576 00000-0 29279-2 0 9999
2 42200 82.9775 132.4546 0070192 16.8642 343.4838 14.02000513510970
| Epoch (UTC): | 29 November 2023 18:57:53 |
| Eccentricity: | 0.0070192 |
| inclination: | 82.9775° |
| perigee height: | 836 km |
| apogee height: | 938 km |
| right ascension of ascending node: | 132.4546° |
| argument of perigee: | 16.8642° |
| revolutions per day: | 14.02000513 |
| mean anomaly at epoch: | 343.4838° |
| orbit number at epoch: | 51097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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