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 12458U 26106.74425186 +.00000000 +00000-0 +50808-4 0 00000
2 12458 89.8432 89.5401 0015992 115.9587 58.0346 13.23292233 01
| Epoch (UTC): | 16 April 2026 17:51:43 |
| Eccentricity: | 0.0015992 |
| inclination: | 89.8432° |
| perigee height: | 1160 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 89.5401° |
| argument of perigee: | 115.9587° |
| revolutions per day: | 13.23292233 |
| mean anomaly at epoch: | 58.0346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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