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 26073.42281307 +.00000000 +00000-0 +30428-4 0 00004
2 27006 99.7686 239.3830 0014175 337.8339 76.2249 13.71092323 05
| Epoch (UTC): | 14 March 2026 10:08:51 |
| Eccentricity: | 0.0014175 |
| inclination: | 99.7686° |
| perigee height: | 985 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 239.3830° |
| argument of perigee: | 337.8339° |
| revolutions per day: | 13.71092323 |
| mean anomaly at epoch: | 76.2249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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