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 26032.52703101 +.00000000 +00000-0 +39313-4 0 00004
2 44387 98.9024 17.8941 0002246 63.8143 296.3266 14.24317805 08
| Epoch (UTC): | 01 February 2026 12:38:55 |
| Eccentricity: | 0.0002246 |
| inclination: | 98.9024° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 17.8941° |
| argument of perigee: | 63.8143° |
| revolutions per day: | 14.24317805 |
| mean anomaly at epoch: | 296.3266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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