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 04362U 26032.07300132 +.00000000 +00000-0 +42056-4 0 00008
2 04362 99.9611 314.4860 0007247 334.7178 36.5175 13.44747401 03
| Epoch (UTC): | 01 February 2026 01:45:07 |
| Eccentricity: | 0.0007247 |
| inclination: | 99.9611° |
| perigee height: | 1086 km |
| apogee height: | 1097 km |
| right ascension of ascending node: | 314.4860° |
| argument of perigee: | 334.7178° |
| revolutions per day: | 13.44747401 |
| mean anomaly at epoch: | 36.5175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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