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 26020.96556448 +.00000000 +00000-0 +41559-3 0 00007
2 36597 97.9907 45.7608 0052110 54.3254 306.2804 15.01970998 07
| Epoch (UTC): | 20 January 2026 23:10:24 |
| Eccentricity: | 0.0052110 |
| inclination: | 97.9907° |
| perigee height: | 525 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 45.7608° |
| argument of perigee: | 54.3254° |
| revolutions per day: | 15.01970998 |
| mean anomaly at epoch: | 306.2804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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