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 35242U 99025DRA 24358.10576772 .00002135 00000-0 25134-2 0 9996
2 35242 99.9809 42.6976 0307079 344.0109 41.8024 13.51022743819693
| Epoch (UTC): | 23 December 2024 02:32:18 |
| Eccentricity: | 0.0307079 |
| inclination: | 99.9809° |
| perigee height: | 840 km |
| apogee height: | 1297 km |
| right ascension of ascending node: | 42.6976° |
| argument of perigee: | 344.0109° |
| revolutions per day: | 13.51022743 |
| mean anomaly at epoch: | 41.8024° |
| orbit number at epoch: | 81969 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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