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 39661U 87060Y 24277.50172379 .00002917 00000-0 10891-2 0 9992
2 39661 65.0092 314.4269 0020423 261.8316 98.0453 14.33372942547548
| Epoch (UTC): | 03 October 2024 12:02:28 |
| Eccentricity: | 0.0020423 |
| inclination: | 65.0092° |
| perigee height: | 766 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 314.4269° |
| argument of perigee: | 261.8316° |
| revolutions per day: | 14.33372942 |
| mean anomaly at epoch: | 98.0453° |
| orbit number at epoch: | 54754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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