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 41603U 16040E 23274.18533682 .00004113 00000-0 17710-3 0 9997
2 41603 97.1610 294.8642 0010941 307.4727 52.5515 15.23076919403621
| Epoch (UTC): | 01 October 2023 04:26:53 |
| Eccentricity: | 0.0010941 |
| inclination: | 97.1610° |
| perigee height: | 489 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 294.8642° |
| argument of perigee: | 307.4727° |
| revolutions per day: | 15.23076919 |
| mean anomaly at epoch: | 52.5515° |
| orbit number at epoch: | 40362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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