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 26063.07375398 +.00000000 +00000-0 +00000-0 0 00004
2 37372 65.4680 318.0416 0009140 326.8456 92.2248 2.12911092 08
| Epoch (UTC): | 04 March 2026 01:46:12 |
| Eccentricity: | 0.0009140 |
| inclination: | 65.4680° |
| perigee height: | 19122 km |
| apogee height: | 19168 km |
| right ascension of ascending node: | 318.0416° |
| argument of perigee: | 326.8456° |
| revolutions per day: | 2.12911092 |
| mean anomaly at epoch: | 92.2248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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