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 39026U 12072A 23036.92018911 .00039456 00000-0 75903-3 0 9991
2 39026 97.2815 31.6160 0025645 42.8323 317.4919 15.47442656564873
| Epoch (UTC): | 05 February 2023 22:05:04 |
| Eccentricity: | 0.0025645 |
| inclination: | 97.2815° |
| perigee height: | 407 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 31.6160° |
| argument of perigee: | 42.8323° |
| revolutions per day: | 15.47442656 |
| mean anomaly at epoch: | 317.4919° |
| orbit number at epoch: | 56487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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