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 26064.44466524 +.00000000 +00000-0 -57193-4 0 00009
2 27473 63.4168 81.1294 0626216 348.0647 111.7565 12.01428900 06
| Epoch (UTC): | 05 March 2026 10:40:19 |
| Eccentricity: | 0.0626216 |
| inclination: | 63.4168° |
| perigee height: | 1170 km |
| apogee height: | 2179 km |
| right ascension of ascending node: | 81.1294° |
| argument of perigee: | 348.0647° |
| revolutions per day: | 12.01428900 |
| mean anomaly at epoch: | 111.7565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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