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 26029.25122628 +.00000000 +00000-0 +00000-0 0 00005
2 37212 63.4614 106.7056 6754424 261.3370 22.8651 2.00608345 02
| Epoch (UTC): | 29 January 2026 06:01:45 |
| Eccentricity: | 0.6754424 |
| inclination: | 63.4614° |
| perigee height: | 2241 km |
| apogee height: | 38116 km |
| right ascension of ascending node: | 106.7056° |
| argument of perigee: | 261.3370° |
| revolutions per day: | 2.00608345 |
| mean anomaly at epoch: | 22.8651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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