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 27473U 26073.45097904 +.00000000 +00000-0 +67685-3 0 00007
2 27473 63.4183 63.2352 0626642 348.0779 185.3553 12.01429295 00
| Epoch (UTC): | 14 March 2026 10:49:24 |
| Eccentricity: | 0.0626642 |
| inclination: | 63.4183° |
| perigee height: | 1170 km |
| apogee height: | 2179 km |
| right ascension of ascending node: | 63.2352° |
| argument of perigee: | 348.0779° |
| revolutions per day: | 12.01429295 |
| mean anomaly at epoch: | 185.3553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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