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 27609U 26156.33237490 +.00000000 +00000-0 +53992-4 0 00000
2 27609 64.5562 13.3659 0049484 246.0504 113.5414 14.81333419 07
| Epoch (UTC): | 05 June 2026 07:58:37 |
| Eccentricity: | 0.0049484 |
| inclination: | 64.5562° |
| perigee height: | 590 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 13.3659° |
| argument of perigee: | 246.0504° |
| revolutions per day: | 14.81333419 |
| mean anomaly at epoch: | 113.5414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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