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 26064.23351294 +.00000000 +00000-0 +30811-3 0 00008
2 27607 64.5518 90.5545 0075169 281.5083 77.7589 14.82761915 03
| Epoch (UTC): | 05 March 2026 05:36:15 |
| Eccentricity: | 0.0075169 |
| inclination: | 64.5518° |
| perigee height: | 568 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 90.5545° |
| argument of perigee: | 281.5083° |
| revolutions per day: | 14.82761915 |
| mean anomaly at epoch: | 77.7589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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