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 65607U 26145.43501550 +.00000000 +00000-0 +18853-3 0 00006
2 65607 97.4472 214.0044 0002911 145.6353 214.5063 15.05654835 07
| Epoch (UTC): | 25 May 2026 10:26:25 |
| Eccentricity: | 0.0002911 |
| inclination: | 97.4472° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 214.0044° |
| argument of perigee: | 145.6353° |
| revolutions per day: | 15.05654835 |
| mean anomaly at epoch: | 214.5063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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