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 28414U 26145.53131602 +.00000000 +00000-0 +45112-3 0 00007
2 28414 97.6059 163.6913 0003940 199.2956 160.8123 15.06127364 09
| Epoch (UTC): | 25 May 2026 12:45:05 |
| Eccentricity: | 0.0003940 |
| inclination: | 97.6059° |
| perigee height: | 545 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 163.6913° |
| argument of perigee: | 199.2956° |
| revolutions per day: | 15.06127364 |
| mean anomaly at epoch: | 160.8123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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