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 44344U 26145.09096730 +.00000000 +00000-0 +00000-0 0 00004
2 44344 42.3288 359.1230 1967588 5.9564 356.1242 4.54375144 04
| Epoch (UTC): | 25 May 2026 02:10:59 |
| Eccentricity: | 0.1967588 |
| inclination: | 42.3288° |
| perigee height: | 5990 km |
| apogee height: | 12049 km |
| right ascension of ascending node: | 359.1230° |
| argument of perigee: | 5.9564° |
| revolutions per day: | 4.54375144 |
| mean anomaly at epoch: | 356.1242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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