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 43495U 18052A 21251.00338102 0.00000000 00000-0 00000-0 0 02
2 43495 97.3648 6.0862 0002074 29.3004 330.6995 15.25981995 06
| Epoch (UTC): | 08 September 2021 00:04:52 |
| Eccentricity: | 0.0002074 |
| inclination: | 97.3648° |
| perigee height: | 486 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 6.0862° |
| argument of perigee: | 29.3004° |
| revolutions per day: | 15.25981995 |
| mean anomaly at epoch: | 330.6995° |
| 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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