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 59941U 26145.35156990 +.00000000 +00000-0 +18460-5 0 00001
2 59941 43.0011 256.3226 0000761 284.1396 75.9371 15.27577129 00
| Epoch (UTC): | 25 May 2026 08:26:15 |
| Eccentricity: | 0.0000761 |
| inclination: | 43.0011° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 256.3226° |
| argument of perigee: | 284.1396° |
| revolutions per day: | 15.27577129 |
| mean anomaly at epoch: | 75.9371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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