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 49215U 21083AF 24358.12843153 .00000118 00000-0 25727-3 0 9990
2 49215 87.9248 22.0844 0001082 115.2608 244.8637 13.20769657166660
| Epoch (UTC): | 23 December 2024 03:04:56 |
| Eccentricity: | 0.0001082 |
| inclination: | 87.9248° |
| perigee height: | 1181 km |
| apogee height: | 1182 km |
| right ascension of ascending node: | 22.0844° |
| argument of perigee: | 115.2608° |
| revolutions per day: | 13.20769657 |
| mean anomaly at epoch: | 244.8637° |
| orbit number at epoch: | 16666 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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