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 27058U 26104.08915178 +.00000000 +00000-0 -21781-4 0 00001
2 27058 82.5326 242.9433 0003816 135.0493 225.0907 12.62085185 03
| Epoch (UTC): | 14 April 2026 02:08:22 |
| Eccentricity: | 0.0003816 |
| inclination: | 82.5326° |
| perigee height: | 1411 km |
| apogee height: | 1417 km |
| right ascension of ascending node: | 242.9433° |
| argument of perigee: | 135.0493° |
| revolutions per day: | 12.62085185 |
| mean anomaly at epoch: | 225.0907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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