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 64931U 26145.30310843 +.00000000 +00000-0 +85263-3 0 00003
2 64931 53.1612 349.7981 0001271 92.2134 267.9012 15.30204118 08
| Epoch (UTC): | 25 May 2026 07:16:28 |
| Eccentricity: | 0.0001271 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 349.7981° |
| argument of perigee: | 92.2134° |
| revolutions per day: | 15.30204118 |
| mean anomaly at epoch: | 267.9012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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