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 36354U 82025AQ 24355.13256981 .00007767 00000-0 34860-2 0 9992
2 36354 82.4949 298.3374 0008924 253.3090 106.7112 14.22312384102247
| Epoch (UTC): | 20 December 2024 03:10:54 |
| Eccentricity: | 0.0008924 |
| inclination: | 82.4949° |
| perigee height: | 811 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 298.3374° |
| argument of perigee: | 253.3090° |
| revolutions per day: | 14.22312384 |
| mean anomaly at epoch: | 106.7112° |
| orbit number at epoch: | 10224 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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