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 31702U 07027B 24287.77666355 .00014191 00000-0 10767-2 0 9996
2 31702 63.3248 298.3800 0519721 34.3036 329.0470 14.33256243 22502
| Epoch (UTC): | 13 October 2024 18:38:23 |
| Eccentricity: | 0.0519721 |
| inclination: | 63.3248° |
| perigee height: | 409 km |
| apogee height: | 1153 km |
| right ascension of ascending node: | 298.3800° |
| argument of perigee: | 34.3036° |
| revolutions per day: | 14.33256243 |
| mean anomaly at epoch: | 329.0470° |
| orbit number at epoch: | 2250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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