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 4135U 69082DP 24358.20196866 .00001004 00000-0 45948-3 0 9996
2 4135 69.9814 300.6731 0050760 269.6505 89.8798 14.23582501854932
| Epoch (UTC): | 23 December 2024 04:50:50 |
| Eccentricity: | 0.0050760 |
| inclination: | 69.9814° |
| perigee height: | 777 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 300.6731° |
| argument of perigee: | 269.6505° |
| revolutions per day: | 14.23582501 |
| mean anomaly at epoch: | 89.8798° |
| orbit number at epoch: | 85493 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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