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 63690U 26145.61705819 +.00000000 +00000-0 +34736-4 0 00009
2 63690 86.5069 320.8356 0001426 82.6424 277.4872 13.24407776 04
| Epoch (UTC): | 25 May 2026 14:48:33 |
| Eccentricity: | 0.0001426 |
| inclination: | 86.5069° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 320.8356° |
| argument of perigee: | 82.6424° |
| revolutions per day: | 13.24407776 |
| mean anomaly at epoch: | 277.4872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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