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 26158.77085869 +.00000000 +00000-0 +19745-4 0 00008
2 00058 28.3248 187.5128 0164929 129.7961 231.7230 13.46430093 01
| Epoch (UTC): | 07 June 2026 18:30:02 |
| Eccentricity: | 0.0164929 |
| inclination: | 28.3248° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 187.5128° |
| argument of perigee: | 129.7961° |
| revolutions per day: | 13.46430093 |
| mean anomaly at epoch: | 231.7230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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