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 26104.03548571 +.00000000 +00000-0 +37226-4 0 00007
2 03597 34.9935 67.8710 0005091 125.5681 234.5485 14.47327225 09
| Epoch (UTC): | 14 April 2026 00:51:05 |
| Eccentricity: | 0.0005091 |
| inclination: | 34.9935° |
| perigee height: | 731 km |
| apogee height: | 738 km |
| right ascension of ascending node: | 67.8710° |
| argument of perigee: | 125.5681° |
| revolutions per day: | 14.47327225 |
| mean anomaly at epoch: | 234.5485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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