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 65848U 26145.27196477 +.00000000 +00000-0 +79240-3 0 00000
2 65848 53.1601 92.2585 0001166 90.8462 269.2674 15.34411008 06
| Epoch (UTC): | 25 May 2026 06:31:37 |
| Eccentricity: | 0.0001166 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.2585° |
| argument of perigee: | 90.8462° |
| revolutions per day: | 15.34411008 |
| mean anomaly at epoch: | 269.2674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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