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 13499U 76069D 24280.43008765 .00011811 00000-0 25355-2 0 9997
2 13499 74.0556 69.2333 0014678 103.0261 288.4690 14.58596157305512
| Epoch (UTC): | 06 October 2024 10:19:19 |
| Eccentricity: | 0.0014678 |
| inclination: | 74.0556° |
| perigee height: | 687 km |
| apogee height: | 708 km |
| right ascension of ascending node: | 69.2333° |
| argument of perigee: | 103.0261° |
| revolutions per day: | 14.58596157 |
| mean anomaly at epoch: | 288.4690° |
| orbit number at epoch: | 30551 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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