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 65648U 26145.18009259 +.00000000 +00000-0 +11363-2 0 00000
2 65648 53.1602 310.9662 0000937 92.3500 267.7610 15.34416061 03
| Epoch (UTC): | 25 May 2026 04:19:20 |
| Eccentricity: | 0.0000937 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 310.9662° |
| argument of perigee: | 92.3500° |
| revolutions per day: | 15.34416061 |
| mean anomaly at epoch: | 267.7610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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