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 27431U 02024B 23159.11643676 .00000018 00000-0 36354-4 0 9993
2 27431 99.0985 189.3339 0016523 104.0317 256.2691 14.09862227 83742
| Epoch (UTC): | 08 June 2023 02:47:40 |
| Eccentricity: | 0.0016523 |
| inclination: | 99.0985° |
| perigee height: | 848 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 189.3339° |
| argument of perigee: | 104.0317° |
| revolutions per day: | 14.09862227 |
| mean anomaly at epoch: | 256.2691° |
| orbit number at epoch: | 8374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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