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 26041.91240670 +.00000000 +00000-0 +37852-4 0 00009
2 27006 99.7629 207.3612 0015152 58.0156 63.7757 13.71090759 06
| Epoch (UTC): | 10 February 2026 21:53:51 |
| Eccentricity: | 0.0015152 |
| inclination: | 99.7629° |
| perigee height: | 984 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 207.3612° |
| argument of perigee: | 58.0156° |
| revolutions per day: | 13.71090759 |
| mean anomaly at epoch: | 63.7757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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