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 65400U 26145.38537017 +.00000000 +00000-0 +15863-3 0 00006
2 65400 97.4518 16.8005 0002399 82.4604 277.6896 15.05655072 09
| Epoch (UTC): | 25 May 2026 09:14:55 |
| Eccentricity: | 0.0002399 |
| inclination: | 97.4518° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.8005° |
| argument of perigee: | 82.4604° |
| revolutions per day: | 15.05655072 |
| mean anomaly at epoch: | 277.6896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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