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 44002U 26107.19114750 +.00000000 +00000-0 +00000-0 0 00007
2 44002 19.8040 154.4825 4800896 144.3568 260.0375 1.83902617 09
| Epoch (UTC): | 17 April 2026 04:35:15 |
| Eccentricity: | 0.4800896 |
| inclination: | 19.8040° |
| perigee height: | 8253 km |
| apogee height: | 35273 km |
| right ascension of ascending node: | 154.4825° |
| argument of perigee: | 144.3568° |
| revolutions per day: | 1.83902617 |
| mean anomaly at epoch: | 260.0375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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