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 27665U 26138.15811792 +.00000000 +00000-0 +58443-4 0 00001
2 27665 39.5755 78.0303 0009361 211.8323 163.7588 14.29548249 08
| Epoch (UTC): | 18 May 2026 03:47:41 |
| Eccentricity: | 0.0009361 |
| inclination: | 39.5755° |
| perigee height: | 787 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 78.0303° |
| argument of perigee: | 211.8323° |
| revolutions per day: | 14.29548249 |
| mean anomaly at epoch: | 163.7588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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