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 39882U 93016BG 23325.71949167 .00024618 00000-0 66778-2 0 9995
2 39882 70.9462 336.4096 0077010 84.3892 31.9502 14.45781700492439
| Epoch (UTC): | 21 November 2023 17:16:04 |
| Eccentricity: | 0.0077010 |
| inclination: | 70.9462° |
| perigee height: | 684 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 336.4096° |
| argument of perigee: | 84.3892° |
| revolutions per day: | 14.45781700 |
| mean anomaly at epoch: | 31.9502° |
| orbit number at epoch: | 49243 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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