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 26158.82919486 +.00000000 +00000-0 +24586-3 0 00000
2 36597 97.9779 187.7573 0048822 312.2020 47.5065 15.02759548 05
| Epoch (UTC): | 07 June 2026 19:54:02 |
| Eccentricity: | 0.0048822 |
| inclination: | 97.9779° |
| perigee height: | 525 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 187.7573° |
| argument of perigee: | 312.2020° |
| revolutions per day: | 15.02759548 |
| mean anomaly at epoch: | 47.5065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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