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 17974U 87041B 24260.85323653 .00000288 00000-0 16519-3 0 9990
2 17974 71.0063 88.7607 0015710 303.3048 152.5569 14.17489284931721
| Epoch (UTC): | 16 September 2024 20:28:39 |
| Eccentricity: | 0.0015710 |
| inclination: | 71.0063° |
| perigee height: | 822 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 88.7607° |
| argument of perigee: | 303.3048° |
| revolutions per day: | 14.17489284 |
| mean anomaly at epoch: | 152.5569° |
| orbit number at epoch: | 93172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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