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 26018.63383600 +.00000000 +00000-0 +13503-3 0 00004
2 36597 97.9916 43.3601 0052428 62.0930 298.5588 15.01947387 01
| Epoch (UTC): | 18 January 2026 15:12:43 |
| Eccentricity: | 0.0052428 |
| inclination: | 97.9916° |
| perigee height: | 525 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 43.3601° |
| argument of perigee: | 62.0930° |
| revolutions per day: | 15.01947387 |
| mean anomaly at epoch: | 298.5588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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