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 26099.53907285 +.00000000 +00000-0 +00000-0 0 00003
2 37212 63.4555 99.2072 6796893 261.1656 22.5642 2.00593186 04
| Epoch (UTC): | 09 April 2026 12:56:15 |
| Eccentricity: | 0.6796893 |
| inclination: | 63.4555° |
| perigee height: | 2129 km |
| apogee height: | 38231 km |
| right ascension of ascending node: | 99.2072° |
| argument of perigee: | 261.1656° |
| revolutions per day: | 2.00593186 |
| mean anomaly at epoch: | 22.5642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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