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 26131.86324242 +.00000000 +00000-0 -11706-3 0 00009
2 27473 63.4183 307.1869 0629319 348.2055 106.7749 12.01429166 07
| Epoch (UTC): | 11 May 2026 20:43:04 |
| Eccentricity: | 0.0629319 |
| inclination: | 63.4183° |
| perigee height: | 1168 km |
| apogee height: | 2181 km |
| right ascension of ascending node: | 307.1869° |
| argument of perigee: | 348.2055° |
| revolutions per day: | 12.01429166 |
| mean anomaly at epoch: | 106.7749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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