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 64495U 26145.39085409 +.00000000 +00000-0 +61779-3 0 00000
2 64495 53.1587 117.5257 0001315 87.4592 272.6561 15.34413681 07
| Epoch (UTC): | 25 May 2026 09:22:49 |
| Eccentricity: | 0.0001315 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 117.5257° |
| argument of perigee: | 87.4592° |
| revolutions per day: | 15.34413681 |
| mean anomaly at epoch: | 272.6561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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