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 53668U 26145.66668980 +.00000000 +00000-0 +17866-1 0 00007
2 53668 97.6036 28.8602 0001101 72.6384 204.2224 15.38406064 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001101 |
| inclination: | 97.6036° |
| perigee height: | 450 km |
| apogee height: | 452 km |
| right ascension of ascending node: | 28.8602° |
| argument of perigee: | 72.6384° |
| revolutions per day: | 15.38406064 |
| mean anomaly at epoch: | 204.2224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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