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 64919U 26145.29677296 +.00000000 +00000-0 +35748-3 0 00008
2 64919 53.1616 349.7481 0001391 111.4959 248.6190 15.30210205 02
| Epoch (UTC): | 25 May 2026 07:07:21 |
| Eccentricity: | 0.0001391 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 349.7481° |
| argument of perigee: | 111.4959° |
| revolutions per day: | 15.30210205 |
| mean anomaly at epoch: | 248.6190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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