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 00058U 26087.96278113 +.00000000 +00000-0 +37235-4 0 00000
2 00058 28.3272 186.8043 0164881 263.5307 94.6440 13.46427187 03
| Epoch (UTC): | 28 March 2026 23:06:24 |
| Eccentricity: | 0.0164881 |
| inclination: | 28.3272° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 186.8043° |
| argument of perigee: | 263.5307° |
| revolutions per day: | 13.46427187 |
| mean anomaly at epoch: | 94.6440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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