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 44709U 26120.85038409 +.00000000 +00000-0 +00000-0 0 00005
2 44709 54.8842 281.4069 0042405 188.8195 170.9972 1.00251230 01
| Epoch (UTC): | 30 April 2026 20:24:33 |
| Eccentricity: | 0.0042405 |
| inclination: | 54.8842° |
| perigee height: | 35614 km |
| apogee height: | 35971 km |
| right ascension of ascending node: | 281.4069° |
| argument of perigee: | 188.8195° |
| revolutions per day: | 1.00251230 |
| mean anomaly at epoch: | 170.9972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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