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 27004U 01056D 23274.18614341 -.00000010 00000-0 40973-4 0 9990
2 27004 99.6975 61.2674 0020123 159.5752 15.3373 13.70184133 90606
| Epoch (UTC): | 01 October 2023 04:28:02 |
| Eccentricity: | 0.0020123 |
| inclination: | 99.6975° |
| perigee height: | 984 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 61.2674° |
| argument of perigee: | 159.5752° |
| revolutions per day: | 13.70184133 |
| mean anomaly at epoch: | 15.3373° |
| orbit number at epoch: | 9060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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