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 65035U 26145.42928475 +.00000000 +00000-0 +15744-2 0 00004
2 65035 53.1603 297.4275 0000334 139.3154 220.7874 15.34744476 06
| Epoch (UTC): | 25 May 2026 10:18:10 |
| Eccentricity: | 0.0000334 |
| inclination: | 53.1603° |
| perigee height: | 461 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 297.4275° |
| argument of perigee: | 139.3154° |
| revolutions per day: | 15.34744476 |
| mean anomaly at epoch: | 220.7874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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