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 26134.82174421 +.00000000 +00000-0 +21820-4 0 00008
2 00058 28.3297 309.0359 0164940 291.5072 66.7963 13.46429284 05
| Epoch (UTC): | 14 May 2026 19:43:18 |
| Eccentricity: | 0.0164940 |
| inclination: | 28.3297° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 309.0359° |
| argument of perigee: | 291.5072° |
| revolutions per day: | 13.46429284 |
| mean anomaly at epoch: | 66.7963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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