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 27607U 26040.69435650 +.00000000 +00000-0 +25192-3 0 00007
2 27607 64.5529 163.3452 0074472 285.7646 73.5256 14.82670110 09
| Epoch (UTC): | 09 February 2026 16:39:52 |
| Eccentricity: | 0.0074472 |
| inclination: | 64.5529° |
| perigee height: | 569 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 163.3452° |
| argument of perigee: | 285.7646° |
| revolutions per day: | 14.82670110 |
| mean anomaly at epoch: | 73.5256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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