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 44387U 26145.62535779 +.00000000 +00000-0 -31205-4 0 00007
2 44387 98.9142 132.5793 0002389 82.8949 277.2501 14.24358236 05
| Epoch (UTC): | 25 May 2026 15:00:30 |
| Eccentricity: | 0.0002389 |
| inclination: | 98.9142° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 132.5793° |
| argument of perigee: | 82.8949° |
| revolutions per day: | 14.24358236 |
| mean anomaly at epoch: | 277.2501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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