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 31797U 07030A 22248.11368757 0.00000000 00000-0 00000-0 0 06
2 31797 98.1448 199.6667 0000812 23.0330 336.9526 15.28020987 05
| Epoch (UTC): | 05 September 2022 02:43:42 |
| Eccentricity: | 0.0000812 |
| inclination: | 98.1448° |
| perigee height: | 481 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 199.6667° |
| argument of perigee: | 23.0330° |
| revolutions per day: | 15.28020987 |
| mean anomaly at epoch: | 336.9526° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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