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 26104.27506956 +.00000000 +00000-0 +31913-4 0 00000
2 00058 28.3261 104.0303 0164904 38.6045 322.6164 13.46428240 06
| Epoch (UTC): | 14 April 2026 06:36:06 |
| Eccentricity: | 0.0164904 |
| inclination: | 28.3261° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 104.0303° |
| argument of perigee: | 38.6045° |
| revolutions per day: | 13.46428240 |
| mean anomaly at epoch: | 322.6164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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