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 is defined by the following mean orbital elements,
1 03597U 26031.59846052 +.00000000 +00000-0 +99831-4 0 00002
2 03597 34.9931 112.3068 0006113 262.0533 97.9464 14.47283238 09
| Epoch (UTC): | 31 January 2026 14:21:46 |
| Eccentricity: | 0.0006113 |
| inclination: | 34.9931° |
| perigee height: | 730 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 112.3068° |
| argument of perigee: | 262.0533° |
| revolutions per day: | 14.47283238 |
| mean anomaly at epoch: | 97.9464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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