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 26064.16606750 +.00000000 +00000-0 +28295-3 0 00003
2 27607 64.5518 90.7631 0075169 281.5213 77.7459 14.82761054 06
| Epoch (UTC): | 05 March 2026 03:59:08 |
| Eccentricity: | 0.0075169 |
| inclination: | 64.5518° |
| perigee height: | 568 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 90.7631° |
| argument of perigee: | 281.5213° |
| revolutions per day: | 14.82761054 |
| mean anomaly at epoch: | 77.7459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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