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 39816U 87020EQ 24355.77044376 .00003192 00000-0 34917-3 0 9993
2 39816 74.0421 7.9650 0032391 309.5138 50.3180 14.87912061550591
| Epoch (UTC): | 20 December 2024 18:29:26 |
| Eccentricity: | 0.0032391 |
| inclination: | 74.0421° |
| perigee height: | 582 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 7.9650° |
| argument of perigee: | 309.5138° |
| revolutions per day: | 14.87912061 |
| mean anomaly at epoch: | 50.3180° |
| orbit number at epoch: | 55059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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