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 24971U 97057A 24281.41783757 .00001354 00000-0 48484-3 0 9994
2 24971 98.7774 251.6092 0051420 246.8718 112.7043 14.34956056413997
| Epoch (UTC): | 07 October 2024 10:01:41 |
| Eccentricity: | 0.0051420 |
| inclination: | 98.7774° |
| perigee height: | 738 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 251.6092° |
| argument of perigee: | 246.8718° |
| revolutions per day: | 14.34956056 |
| mean anomaly at epoch: | 112.7043° |
| orbit number at epoch: | 41399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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