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 64286U 26145.63198296 +.00000000 +00000-0 +30093-4 0 00000
2 64286 86.5028 21.2227 0001694 88.4210 271.7118 13.24407634 07
| Epoch (UTC): | 25 May 2026 15:10:03 |
| Eccentricity: | 0.0001694 |
| inclination: | 86.5028° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.2227° |
| argument of perigee: | 88.4210° |
| revolutions per day: | 13.24407634 |
| mean anomaly at epoch: | 271.7118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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