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 65071U 26145.48821080 +.00000000 +00000-0 +39941-3 0 00000
2 65071 97.4483 222.5129 0002493 158.5116 201.6216 15.05659487 02
| Epoch (UTC): | 25 May 2026 11:43:01 |
| Eccentricity: | 0.0002493 |
| inclination: | 97.4483° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.5129° |
| argument of perigee: | 158.5116° |
| revolutions per day: | 15.05659487 |
| mean anomaly at epoch: | 201.6216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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