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 26018.39423367 +.00000000 +00000-0 +23543-4 0 00003
2 27006 99.7590 183.4716 0015191 115.3359 262.9240 13.71088848 03
| Epoch (UTC): | 18 January 2026 09:27:41 |
| Eccentricity: | 0.0015191 |
| inclination: | 99.7590° |
| perigee height: | 984 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 183.4716° |
| argument of perigee: | 115.3359° |
| revolutions per day: | 13.71088848 |
| mean anomaly at epoch: | 262.9240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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