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 26070.77051860 +.00000000 +00000-0 +58375-4 0 00009
2 04362 99.9606 352.8076 0006880 232.6016 182.6894 13.44749923 03
| Epoch (UTC): | 11 March 2026 18:29:32 |
| Eccentricity: | 0.0006880 |
| inclination: | 99.9606° |
| perigee height: | 1086 km |
| apogee height: | 1097 km |
| right ascension of ascending node: | 352.8076° |
| argument of perigee: | 232.6016° |
| revolutions per day: | 13.44749923 |
| mean anomaly at epoch: | 182.6894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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