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 64508U 26145.22800031 +.00000000 +00000-0 +88031-4 0 00004
2 64508 51.8978 237.1212 0000289 110.4808 249.6186 14.79935115 03
| Epoch (UTC): | 25 May 2026 05:28:19 |
| Eccentricity: | 0.0000289 |
| inclination: | 51.8978° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 237.1212° |
| argument of perigee: | 110.4808° |
| revolutions per day: | 14.79935115 |
| mean anomaly at epoch: | 249.6186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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