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 23088.93102694 .00003984 00000-0 17738-3 0 9993
2 41603 97.1753 118.1459 0011343 230.5700 224.8393 15.21956636375433
| Epoch (UTC): | 29 March 2023 22:20:40 |
| Eccentricity: | 0.0011343 |
| inclination: | 97.1753° |
| perigee height: | 492 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 118.1459° |
| argument of perigee: | 230.5700° |
| revolutions per day: | 15.21956636 |
| mean anomaly at epoch: | 224.8393° |
| orbit number at epoch: | 37543 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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