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 32790U 26053.87767854 +.00000000 +00000-0 +43884-3 0 00002
2 32790 97.8544 31.5841 0012191 72.7218 287.5341 15.04612943 08
| Epoch (UTC): | 22 February 2026 21:03:51 |
| Eccentricity: | 0.0012191 |
| inclination: | 97.8544° |
| perigee height: | 544 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 31.5841° |
| argument of perigee: | 72.7218° |
| revolutions per day: | 15.04612943 |
| mean anomaly at epoch: | 287.5341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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