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 64211U 26145.12575391 +.00000000 +00000-0 +73844-3 0 00007
2 64211 53.1598 44.1927 0001305 87.5884 272.5266 15.30201880 01
| Epoch (UTC): | 25 May 2026 03:01:05 |
| Eccentricity: | 0.0001305 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.1927° |
| argument of perigee: | 87.5884° |
| revolutions per day: | 15.30201880 |
| mean anomaly at epoch: | 272.5266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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