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 26017.63451436 +.00000000 +00000-0 +99056-4 0 00004
2 36597 97.9923 42.3309 0052616 65.3606 295.3085 15.01943985 05
| Epoch (UTC): | 17 January 2026 15:13:42 |
| Eccentricity: | 0.0052616 |
| inclination: | 97.9923° |
| perigee height: | 524 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 42.3309° |
| argument of perigee: | 65.3606° |
| revolutions per day: | 15.01943985 |
| mean anomaly at epoch: | 295.3085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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