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 64479U 26145.63875736 +.00000000 +00000-0 +79545-3 0 00009
2 64479 53.1596 116.9661 0001377 93.2419 266.8742 15.35418499 01
| Epoch (UTC): | 25 May 2026 15:19:48 |
| Eccentricity: | 0.0001377 |
| inclination: | 53.1596° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 116.9661° |
| argument of perigee: | 93.2419° |
| revolutions per day: | 15.35418499 |
| mean anomaly at epoch: | 266.8742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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