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 27605U 26154.54539080 +.00000000 +00000-0 +91652-4 0 00002
2 27605 64.5517 172.4743 0079065 265.6400 93.5667 14.79429341 08
| Epoch (UTC): | 03 June 2026 13:05:21 |
| Eccentricity: | 0.0079065 |
| inclination: | 64.5517° |
| perigee height: | 576 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 172.4743° |
| argument of perigee: | 265.6400° |
| revolutions per day: | 14.79429341 |
| mean anomaly at epoch: | 93.5667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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