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 26077.97750565 +.00000000 +00000-0 -35830-4 0 00009
2 44387 98.9093 63.9573 0000381 332.7444 27.3714 14.24337319 09
| Epoch (UTC): | 18 March 2026 23:27:36 |
| Eccentricity: | 0.0000381 |
| inclination: | 98.9093° |
| perigee height: | 810 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 63.9573° |
| argument of perigee: | 332.7444° |
| revolutions per day: | 14.24337319 |
| mean anomaly at epoch: | 27.3714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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