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 44785U 26145.61483662 +.00000000 +00000-0 +13951-3 0 00007
2 44785 88.9258 225.0313 0011620 164.1006 196.0515 13.56040920 01
| Epoch (UTC): | 25 May 2026 14:45:21 |
| Eccentricity: | 0.0011620 |
| inclination: | 88.9258° |
| perigee height: | 1041 km |
| apogee height: | 1059 km |
| right ascension of ascending node: | 225.0313° |
| argument of perigee: | 164.1006° |
| revolutions per day: | 13.56040920 |
| mean anomaly at epoch: | 196.0515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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