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 27664U 26087.64309943 +.00000000 +00000-0 +29742-3 0 00006
2 27664 39.7458 179.4778 0149263 239.3188 119.2813 14.89911304 00
| Epoch (UTC): | 28 March 2026 15:26:03 |
| Eccentricity: | 0.0149263 |
| inclination: | 39.7458° |
| perigee height: | 494 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 179.4778° |
| argument of perigee: | 239.3188° |
| revolutions per day: | 14.89911304 |
| mean anomaly at epoch: | 119.2813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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