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 26722U 01011D 23033.90421549 .00000114 00000-0 10656-1 0 9992
2 26722 2.2738 15.8347 7060028 20.3221 357.0490 2.22907659178459
| Epoch (UTC): | 02 February 2023 21:42:04 |
| Eccentricity: | 0.7060028 |
| inclination: | 2.2738° |
| perigee height: | 899 km |
| apogee height: | 35852 km |
| right ascension of ascending node: | 15.8347° |
| argument of perigee: | 20.3221° |
| revolutions per day: | 2.22907659 |
| mean anomaly at epoch: | 357.0490° |
| orbit number at epoch: | 17845 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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