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 31361U 99025BRR 25321.22137491 .00000390 00000-0 20974-3 0 9998
2 31361 98.5477 297.4865 0045688 142.7192 217.7170 14.17726165962028
| Epoch (UTC): | 17 November 2025 05:18:46 |
| Eccentricity: | 0.0045688 |
| inclination: | 98.5477° |
| perigee height: | 800 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 297.4865° |
| argument of perigee: | 142.7192° |
| revolutions per day: | 14.17726165 |
| mean anomaly at epoch: | 217.7170° |
| orbit number at epoch: | 96202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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