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 4149U 69082T 24358.36940197 .00001048 00000-0 52424-3 0 9997
2 4149 70.3059 45.1517 0032826 104.0452 256.4321 14.19037692842362
| Epoch (UTC): | 23 December 2024 08:51:56 |
| Eccentricity: | 0.0032826 |
| inclination: | 70.3059° |
| perigee height: | 805 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 45.1517° |
| argument of perigee: | 104.0452° |
| revolutions per day: | 14.19037692 |
| mean anomaly at epoch: | 256.4321° |
| orbit number at epoch: | 84236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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