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 36597U 26040.68397865 +.00000000 +00000-0 +29205-3 0 00008
2 36597 97.9915 66.0659 0050242 348.1559 11.8479 15.02140929 05
| Epoch (UTC): | 09 February 2026 16:24:55 |
| Eccentricity: | 0.0050242 |
| inclination: | 97.9915° |
| perigee height: | 525 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 66.0659° |
| argument of perigee: | 348.1559° |
| revolutions per day: | 15.02140929 |
| mean anomaly at epoch: | 11.8479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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