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 65801U 26145.11894161 +.00000000 +00000-0 +49513-3 0 00007
2 65801 97.4506 7.9637 0001703 94.4743 265.6679 15.05660292 04
| Epoch (UTC): | 25 May 2026 02:51:16 |
| Eccentricity: | 0.0001703 |
| inclination: | 97.4506° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 7.9637° |
| argument of perigee: | 94.4743° |
| revolutions per day: | 15.05660292 |
| mean anomaly at epoch: | 265.6679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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