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 26075.90132515 +.00000000 +00000-0 +20166-3 0 00009
2 27607 64.5530 54.4672 0075337 279.3752 79.8842 14.82814680 05
| Epoch (UTC): | 16 March 2026 21:37:54 |
| Eccentricity: | 0.0075337 |
| inclination: | 64.5530° |
| perigee height: | 568 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 54.4672° |
| argument of perigee: | 279.3752° |
| revolutions per day: | 14.82814680 |
| mean anomaly at epoch: | 79.8842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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