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 31122U 07012F 23335.84616833 .00006402 00000-0 11646-2 0 9996
2 31122 98.3291 298.5428 0072639 311.5001 47.9981 14.64763637885230
| Epoch (UTC): | 01 December 2023 20:18:28 |
| Eccentricity: | 0.0072639 |
| inclination: | 98.3291° |
| perigee height: | 626 km |
| apogee height: | 729 km |
| right ascension of ascending node: | 298.5428° |
| argument of perigee: | 311.5001° |
| revolutions per day: | 14.64763637 |
| mean anomaly at epoch: | 47.9981° |
| orbit number at epoch: | 88523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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