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 27940U 26068.49009207 +.00000000 +00000-0 +15857-3 0 00007
2 27940 98.3813 243.8289 0012154 314.7262 45.2953 14.69367712 04
| Epoch (UTC): | 09 March 2026 11:45:43 |
| Eccentricity: | 0.0012154 |
| inclination: | 98.3813° |
| perigee height: | 655 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 243.8289° |
| argument of perigee: | 314.7262° |
| revolutions per day: | 14.69367712 |
| mean anomaly at epoch: | 45.2953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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