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 27608U 26150.76085405 +.00000000 +00000-0 +14442-3 0 00003
2 27608 64.5522 75.4623 0061852 256.0525 103.3698 14.84271109 00
| Epoch (UTC): | 30 May 2026 18:15:37 |
| Eccentricity: | 0.0061852 |
| inclination: | 64.5522° |
| perigee height: | 573 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 75.4623° |
| argument of perigee: | 256.0525° |
| revolutions per day: | 14.84271109 |
| mean anomaly at epoch: | 103.3698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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