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 64803U 26145.46955602 +.00000000 +00000-0 +24419-3 0 00002
2 64803 70.0005 301.0227 0002903 264.5663 95.5165 14.98336153 00
| Epoch (UTC): | 25 May 2026 11:16:09 |
| Eccentricity: | 0.0002903 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.0227° |
| argument of perigee: | 264.5663° |
| revolutions per day: | 14.98336153 |
| mean anomaly at epoch: | 95.5165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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