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 65337U 26145.46707497 +.00000000 +00000-0 +31748-3 0 00005
2 65337 53.1574 209.9847 0001094 84.0623 276.0503 15.30198428 01
| Epoch (UTC): | 25 May 2026 11:12:35 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.9847° |
| argument of perigee: | 84.0623° |
| revolutions per day: | 15.30198428 |
| mean anomaly at epoch: | 276.0503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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