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 43797U 26145.02461145 +.00000000 +00000-0 +29095-3 0 00002
2 43797 96.9279 169.2064 0002743 202.3350 157.7782 15.48056080 07
| Epoch (UTC): | 25 May 2026 00:35:26 |
| Eccentricity: | 0.0002743 |
| inclination: | 96.9279° |
| perigee height: | 421 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 169.2064° |
| argument of perigee: | 202.3350° |
| revolutions per day: | 15.48056080 |
| mean anomaly at epoch: | 157.7782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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