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 26133.42366705 +.00000000 +00000-0 +34289-4 0 00005
2 03597 34.9936 263.7861 0005711 349.7178 10.3395 14.47338785 07
| Epoch (UTC): | 13 May 2026 10:10:04 |
| Eccentricity: | 0.0005711 |
| inclination: | 34.9936° |
| perigee height: | 730 km |
| apogee height: | 738 km |
| right ascension of ascending node: | 263.7861° |
| argument of perigee: | 349.7178° |
| revolutions per day: | 14.47338785 |
| mean anomaly at epoch: | 10.3395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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