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 12627U 26150.41723088 +.00000000 +00000-0 +00000-0 0 00008
2 12627 68.5865 92.9461 6012683 352.7638 275.2166 1.98064572 00
| Epoch (UTC): | 30 May 2026 10:00:48 |
| Eccentricity: | 0.6012683 |
| inclination: | 68.5865° |
| perigee height: | 4301 km |
| apogee height: | 36509 km |
| right ascension of ascending node: | 92.9461° |
| argument of perigee: | 352.7638° |
| revolutions per day: | 1.98064572 |
| mean anomaly at epoch: | 275.2166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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