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 34948U 93036AEB 24263.26063837 .00068431 00000-0 86011-2 0 9991
2 34948 74.0070 228.5784 0008628 355.5491 69.5236 14.81678602814209
| Epoch (UTC): | 19 September 2024 06:15:19 |
| Eccentricity: | 0.0008628 |
| inclination: | 74.0070° |
| perigee height: | 618 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 228.5784° |
| argument of perigee: | 355.5491° |
| revolutions per day: | 14.81678602 |
| mean anomaly at epoch: | 69.5236° |
| orbit number at epoch: | 81420 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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