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 26134.93401009 +.00000000 +00000-0 +00000-0 0 00000
2 37212 63.4516 95.3748 6818630 261.0998 22.3817 2.00588399 02
| Epoch (UTC): | 14 May 2026 22:24:58 |
| Eccentricity: | 0.6818630 |
| inclination: | 63.4516° |
| perigee height: | 2071 km |
| apogee height: | 38289 km |
| right ascension of ascending node: | 95.3748° |
| argument of perigee: | 261.0998° |
| revolutions per day: | 2.00588399 |
| mean anomaly at epoch: | 22.3817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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