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 26133.56127824 +.00000000 +00000-0 +22563-4 0 00008
2 00058 28.3299 315.4312 0164942 281.0728 77.1309 13.46429237 09
| Epoch (UTC): | 13 May 2026 13:28:14 |
| Eccentricity: | 0.0164942 |
| inclination: | 28.3299° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 315.4312° |
| argument of perigee: | 281.0728° |
| revolutions per day: | 13.46429237 |
| mean anomaly at epoch: | 77.1309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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