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 08800U 76032B 24287.09465931 .00000338 00000-0 17540-3 0 9998
2 08800 81.2482 134.6260 0094091 170.2620 190.0404 14.10474723494981
| Epoch (UTC): | 13 October 2024 02:16:18 |
| Eccentricity: | 0.0094091 |
| inclination: | 81.2482° |
| perigee height: | 789 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 134.6260° |
| argument of perigee: | 170.2620° |
| revolutions per day: | 14.10474723 |
| mean anomaly at epoch: | 190.0404° |
| orbit number at epoch: | 49498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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