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 37212U 26157.86626302 +.00000000 +00000-0 +00000-0 0 00002
2 37212 63.4468 92.8691 6832469 261.0608 22.2492 2.00587054 06
| Epoch (UTC): | 06 June 2026 20:47:25 |
| Eccentricity: | 0.6832469 |
| inclination: | 63.4468° |
| perigee height: | 2034 km |
| apogee height: | 38326 km |
| right ascension of ascending node: | 92.8691° |
| argument of perigee: | 261.0608° |
| revolutions per day: | 2.00587054 |
| mean anomaly at epoch: | 22.2492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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