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 64812U 26145.39444334 +.00000000 +00000-0 +35988-3 0 00002
2 64812 70.0002 301.1179 0002537 268.6530 91.4339 14.98343049 05
| Epoch (UTC): | 25 May 2026 09:27:59 |
| Eccentricity: | 0.0002537 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.1179° |
| argument of perigee: | 268.6530° |
| revolutions per day: | 14.98343049 |
| mean anomaly at epoch: | 91.4339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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