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 26129.51543103 +.00000000 +00000-0 +11698-3 0 00005
2 27607 64.5524 248.6252 0075631 269.5316 89.7123 14.82964537 02
| Epoch (UTC): | 09 May 2026 12:22:13 |
| Eccentricity: | 0.0075631 |
| inclination: | 64.5524° |
| perigee height: | 567 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 248.6252° |
| argument of perigee: | 269.5316° |
| revolutions per day: | 14.82964537 |
| mean anomaly at epoch: | 89.7123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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