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 65285U 26145.41302397 +.00000000 +00000-0 +32627-3 0 00009
2 65285 97.4484 197.8874 0002137 119.0862 241.0579 15.05657537 00
| Epoch (UTC): | 25 May 2026 09:54:45 |
| Eccentricity: | 0.0002137 |
| inclination: | 97.4484° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 197.8874° |
| argument of perigee: | 119.0862° |
| revolutions per day: | 15.05657537 |
| mean anomaly at epoch: | 241.0579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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