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 09444U 26088.16151946 +.00000000 +00000-0 +72340-4 0 00001
2 09444 74.0510 154.0212 0013825 225.4772 134.5254 14.39349870 05
| Epoch (UTC): | 29 March 2026 03:52:35 |
| Eccentricity: | 0.0013825 |
| inclination: | 74.0510° |
| perigee height: | 751 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 154.0212° |
| argument of perigee: | 225.4772° |
| revolutions per day: | 14.39349870 |
| mean anomaly at epoch: | 134.5254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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