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 27939U 03042A 24280.90572479 .00006624 00000-0 10912-2 0 9991
2 27939 98.3053 79.0243 0012671 69.6304 83.6583 14.70795192124566
| Epoch (UTC): | 06 October 2024 21:44:14 |
| Eccentricity: | 0.0012671 |
| inclination: | 98.3053° |
| perigee height: | 649 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 79.0243° |
| argument of perigee: | 69.6304° |
| revolutions per day: | 14.70795192 |
| mean anomaly at epoch: | 83.6583° |
| orbit number at epoch: | 12456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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