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 41652U 00055NR 24357.03166114 .00019726 00000-0 75506-2 0 9991
2 41652 98.8822 83.7334 0041138 233.3859 126.3536 14.30153694447046
| Epoch (UTC): | 22 December 2024 00:45:35 |
| Eccentricity: | 0.0041138 |
| inclination: | 98.8822° |
| perigee height: | 762 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 83.7334° |
| argument of perigee: | 233.3859° |
| revolutions per day: | 14.30153694 |
| mean anomaly at epoch: | 126.3536° |
| orbit number at epoch: | 44704 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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