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 44836U 26145.64140321 +.00000000 +00000-0 +25814-3 0 00000
2 44836 97.4888 217.7777 0014976 44.2652 315.9778 15.20413253 05
| Epoch (UTC): | 25 May 2026 15:23:37 |
| Eccentricity: | 0.0014976 |
| inclination: | 97.4888° |
| perigee height: | 494 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 217.7777° |
| argument of perigee: | 44.2652° |
| revolutions per day: | 15.20413253 |
| mean anomaly at epoch: | 315.9778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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