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 65336U 26145.37971253 +.00000000 +00000-0 +36361-3 0 00003
2 65336 53.1586 210.8634 0000913 52.8725 307.2359 15.30198409 08
| Epoch (UTC): | 25 May 2026 09:06:47 |
| Eccentricity: | 0.0000913 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.8634° |
| argument of perigee: | 52.8725° |
| revolutions per day: | 15.30198409 |
| mean anomaly at epoch: | 307.2359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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