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 44059U 26145.50476094 +.00000000 +00000-0 +10825-4 0 00008
2 44059 87.9105 233.2799 0002169 106.7879 253.3490 13.16594475 06
| Epoch (UTC): | 25 May 2026 12:06:51 |
| Eccentricity: | 0.0002169 |
| inclination: | 87.9105° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2799° |
| argument of perigee: | 106.7879° |
| revolutions per day: | 13.16594475 |
| mean anomaly at epoch: | 253.3490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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