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 26042.01622441 +.00000000 +00000-0 +28764-3 0 00007
2 36597 97.9917 67.4383 0050143 343.6912 16.2695 15.02151393 05
| Epoch (UTC): | 11 February 2026 00:23:21 |
| Eccentricity: | 0.0050143 |
| inclination: | 97.9917° |
| perigee height: | 525 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 67.4383° |
| argument of perigee: | 343.6912° |
| revolutions per day: | 15.02151393 |
| mean anomaly at epoch: | 16.2695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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