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 44634U 26145.39841138 +.00000000 +00000-0 -48825-3 0 00000
2 44634 87.8852 284.2995 0010837 122.7038 237.5137 13.11904159 04
| Epoch (UTC): | 25 May 2026 09:33:42 |
| Eccentricity: | 0.0010837 |
| inclination: | 87.8852° |
| perigee height: | 1208 km |
| apogee height: | 1224 km |
| right ascension of ascending node: | 284.2995° |
| argument of perigee: | 122.7038° |
| revolutions per day: | 13.11904159 |
| mean anomaly at epoch: | 237.5137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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