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 65202U 26145.32286404 +.00000000 +00000-0 +73428-3 0 00002
2 65202 53.1575 156.0490 0001182 93.5613 266.5525 15.34409555 09
| Epoch (UTC): | 25 May 2026 07:44:55 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.1575° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 156.0490° |
| argument of perigee: | 93.5613° |
| revolutions per day: | 15.34409555 |
| mean anomaly at epoch: | 266.5525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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