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 24278.51316663 .00006968 00000-0 11482-2 0 9990
2 27939 98.3046 76.5862 0012738 76.6732 16.0510 14.70765380124346
| Epoch (UTC): | 04 October 2024 12:18:57 |
| Eccentricity: | 0.0012738 |
| inclination: | 98.3046° |
| perigee height: | 649 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 76.5862° |
| argument of perigee: | 76.6732° |
| revolutions per day: | 14.70765380 |
| mean anomaly at epoch: | 16.0510° |
| orbit number at epoch: | 12434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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