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 41724U 16047A 23059.61765327 0.00000000 00000-0 00000-0 0 05
2 41724 2.4550 10.4990 0003090 320.1047 39.8953 1.00270000 05
| Epoch (UTC): | 28 February 2023 14:49:25 |
| Eccentricity: | 0.0003090 |
| inclination: | 2.4550° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 10.4990° |
| argument of perigee: | 320.1047° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 39.8953° |
| 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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