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 37372U 26109.72669644 +.00000000 +00000-0 +00000-0 0 00007
2 37372 65.4406 316.4640 0008574 330.0291 207.3697 2.12911258 00
| Epoch (UTC): | 19 April 2026 17:26:26 |
| Eccentricity: | 0.0008574 |
| inclination: | 65.4406° |
| perigee height: | 19123 km |
| apogee height: | 19167 km |
| right ascension of ascending node: | 316.4640° |
| argument of perigee: | 330.0291° |
| revolutions per day: | 2.12911258 |
| mean anomaly at epoch: | 207.3697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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