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 26039.47269793 +.00000000 +00000-0 +18575-4 0 00003
2 00058 28.3285 72.8471 0164750 221.9482 136.8338 13.46424105 05
| Epoch (UTC): | 08 February 2026 11:20:41 |
| Eccentricity: | 0.0164750 |
| inclination: | 28.3285° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 72.8471° |
| argument of perigee: | 221.9482° |
| revolutions per day: | 13.46424105 |
| mean anomaly at epoch: | 136.8338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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