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 26159.03047475 +.00000000 +00000-0 +22310-4 0 00003
2 27006 99.7792 326.4444 0015273 114.2659 354.1096 13.71094473 00
| Epoch (UTC): | 08 June 2026 00:43:53 |
| Eccentricity: | 0.0015273 |
| inclination: | 99.7792° |
| perigee height: | 984 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 326.4444° |
| argument of perigee: | 114.2659° |
| revolutions per day: | 13.71094473 |
| mean anomaly at epoch: | 354.1096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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