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 31129U 07012N 23272.38570572 .00002551 00000-0 52022-3 0 9996
2 31129 98.3239 219.3591 0089955 272.3115 86.7787 14.59342487873726
| Epoch (UTC): | 29 September 2023 09:15:24 |
| Eccentricity: | 0.0089955 |
| inclination: | 98.3239° |
| perigee height: | 631 km |
| apogee height: | 759 km |
| right ascension of ascending node: | 219.3591° |
| argument of perigee: | 272.3115° |
| revolutions per day: | 14.59342487 |
| mean anomaly at epoch: | 86.7787° |
| orbit number at epoch: | 87372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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