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 26039.17613391 +.00000000 +00000-0 +42846-4 0 00005
2 00058 28.3284 74.3519 0164746 219.4955 139.3479 13.46424201 07
| Epoch (UTC): | 08 February 2026 04:13:37 |
| Eccentricity: | 0.0164746 |
| inclination: | 28.3284° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 74.3519° |
| argument of perigee: | 219.4955° |
| revolutions per day: | 13.46424201 |
| mean anomaly at epoch: | 139.3479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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