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 26106.88842829 +.00000000 +00000-0 +46227-4 0 00002
2 27605 64.5537 319.0751 0079068 274.4951 84.7124 14.79372551 00
| Epoch (UTC): | 16 April 2026 21:19:20 |
| Eccentricity: | 0.0079068 |
| inclination: | 64.5537° |
| perigee height: | 576 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 319.0751° |
| argument of perigee: | 274.4951° |
| revolutions per day: | 14.79372551 |
| mean anomaly at epoch: | 84.7124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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