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 26067.08491968 +.00000000 +00000-0 +28202-4 0 00002
2 27006 99.7675 232.9409 0014380 354.4086 112.5080 13.71092113 00
| Epoch (UTC): | 08 March 2026 02:02:17 |
| Eccentricity: | 0.0014380 |
| inclination: | 99.7675° |
| perigee height: | 985 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 232.9409° |
| argument of perigee: | 354.4086° |
| revolutions per day: | 13.71092113 |
| mean anomaly at epoch: | 112.5080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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