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 44112U 26145.42447637 +.00000000 +00000-0 +00000-0 0 00000
2 44112 0.0526 0.0731 0002502 54.6432 305.3067 5.00115575 04
| Epoch (UTC): | 25 May 2026 10:11:14 |
| Eccentricity: | 0.0002502 |
| inclination: | 0.0526° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 0.0731° |
| argument of perigee: | 54.6432° |
| revolutions per day: | 5.00115575 |
| mean anomaly at epoch: | 305.3067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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