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 34998U 93036AFW 24278.38881390 .00010749 00000-0 30087-2 0 9998
2 34998 74.0112 254.2031 0019967 148.9684 1.5697 14.46063539811334
| Epoch (UTC): | 04 October 2024 09:19:53 |
| Eccentricity: | 0.0019967 |
| inclination: | 74.0112° |
| perigee height: | 724 km |
| apogee height: | 753 km |
| right ascension of ascending node: | 254.2031° |
| argument of perigee: | 148.9684° |
| revolutions per day: | 14.46063539 |
| mean anomaly at epoch: | 1.5697° |
| orbit number at epoch: | 81133 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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