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 26065.44752583 +.00000000 +00000-0 +30257-3 0 00002
2 27607 64.5519 86.7998 0075186 281.2996 77.9668 14.82767672 08
| Epoch (UTC): | 06 March 2026 10:44:26 |
| Eccentricity: | 0.0075186 |
| inclination: | 64.5519° |
| perigee height: | 568 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 86.7998° |
| argument of perigee: | 281.2996° |
| revolutions per day: | 14.82767672 |
| mean anomaly at epoch: | 77.9668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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