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 26106.51900138 +.00000000 +00000-0 +34959-4 0 00003
2 03597 34.9939 54.0045 0005263 147.0442 213.0578 14.47327926 00
| Epoch (UTC): | 16 April 2026 12:27:21 |
| Eccentricity: | 0.0005263 |
| inclination: | 34.9939° |
| perigee height: | 731 km |
| apogee height: | 738 km |
| right ascension of ascending node: | 54.0045° |
| argument of perigee: | 147.0442° |
| revolutions per day: | 14.47327926 |
| mean anomaly at epoch: | 213.0578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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