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 65452U 26145.56693676 +.00000000 +00000-0 +27564-3 0 00008
2 65452 97.4537 359.7569 0003275 83.2547 276.9053 15.05659565 08
| Epoch (UTC): | 25 May 2026 13:36:23 |
| Eccentricity: | 0.0003275 |
| inclination: | 97.4537° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 359.7569° |
| argument of perigee: | 83.2547° |
| revolutions per day: | 15.05659565 |
| mean anomaly at epoch: | 276.9053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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