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 39444U 13066AE 23090.16753551 .00008021 00000-0 90337-3 0 9993
2 39444 97.6637 57.1307 0054204 168.0330 192.2187 14.85809909504645
| Epoch (UTC): | 31 March 2023 04:01:15 |
| Eccentricity: | 0.0054204 |
| inclination: | 97.6637° |
| perigee height: | 573 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 57.1307° |
| argument of perigee: | 168.0330° |
| revolutions per day: | 14.85809909 |
| mean anomaly at epoch: | 192.2187° |
| orbit number at epoch: | 50464 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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