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 65201U 26145.45103289 +.00000000 +00000-0 +50729-3 0 00003
2 65201 53.1575 155.4227 0001077 91.8076 268.3050 15.34421292 01
| Epoch (UTC): | 25 May 2026 10:49:29 |
| Eccentricity: | 0.0001077 |
| inclination: | 53.1575° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 155.4227° |
| argument of perigee: | 91.8076° |
| revolutions per day: | 15.34421292 |
| mean anomaly at epoch: | 268.3050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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