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 27006U 26160.21142588 +.00000000 +00000-0 +24587-4 0 00004
2 27006 99.7793 327.6458 0015298 111.3407 63.1088 13.71094507 01
| Epoch (UTC): | 09 June 2026 05:04:27 |
| Eccentricity: | 0.0015298 |
| inclination: | 99.7793° |
| perigee height: | 984 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 327.6458° |
| argument of perigee: | 111.3407° |
| revolutions per day: | 13.71094507 |
| mean anomaly at epoch: | 63.1088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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