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 44061U 26145.29761733 +.00000000 +00000-0 +18495-3 0 00004
2 44061 87.9000 263.7444 0001738 98.2500 261.8827 13.15551002 01
| Epoch (UTC): | 25 May 2026 07:08:34 |
| Eccentricity: | 0.0001738 |
| inclination: | 87.9000° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7444° |
| argument of perigee: | 98.2500° |
| revolutions per day: | 13.15551002 |
| mean anomaly at epoch: | 261.8827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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