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 23246.97056390 0.00000000 00000-0 00000-0 0 00
2 43495 97.3657 1.6190 0002061 349.2960 10.6690 15.25981530 04
| Epoch (UTC): | 03 September 2023 23:17:36 |
| Eccentricity: | 0.0002061 |
| inclination: | 97.3657° |
| perigee height: | 486 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 1.6190° |
| argument of perigee: | 349.2960° |
| revolutions per day: | 15.25981530 |
| mean anomaly at epoch: | 10.6690° |
| 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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