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 31698U 07026A 22267.45717369 -.00002008 00000-0 -92511-4 0 9997
2 31698 97.4488 273.6546 0001998 97.1034 45.5371 15.19133199847144
| Epoch (UTC): | 24 September 2022 10:58:19 |
| Eccentricity: | 0.0001998 |
| inclination: | 97.4488° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 273.6546° |
| argument of perigee: | 97.1034° |
| revolutions per day: | 15.19133199 |
| mean anomaly at epoch: | 45.5371° |
| orbit number at epoch: | 84714 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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