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 64607U 26144.98913142 +.00000000 +00000-0 +49288-3 0 00004
2 64607 53.1596 350.9863 0000739 43.4519 316.6539 15.30211092 00
| Epoch (UTC): | 24 May 2026 23:44:20 |
| Eccentricity: | 0.0000739 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 350.9863° |
| argument of perigee: | 43.4519° |
| revolutions per day: | 15.30211092 |
| mean anomaly at epoch: | 316.6539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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