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 27945U 26106.69206851 +.00000000 +00000-0 +46894-4 0 00007
2 27945 98.3786 274.0204 0011750 165.2735 194.8813 14.67835610 07
| Epoch (UTC): | 16 April 2026 16:36:34 |
| Eccentricity: | 0.0011750 |
| inclination: | 98.3786° |
| perigee height: | 660 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 274.0204° |
| argument of perigee: | 165.2735° |
| revolutions per day: | 14.67835610 |
| mean anomaly at epoch: | 194.8813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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