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 64284U 26145.64740307 +.00000000 +00000-0 +55926-4 0 00007
2 64284 86.5029 21.2337 0001722 88.5028 271.6303 13.24412165 08
| Epoch (UTC): | 25 May 2026 15:32:15 |
| Eccentricity: | 0.0001722 |
| inclination: | 86.5029° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.2337° |
| argument of perigee: | 88.5028° |
| revolutions per day: | 13.24412165 |
| mean anomaly at epoch: | 271.6303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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