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 59390U 26145.58360024 +.00000000 +00000-0 +12429-4 0 00007
2 59390 53.1601 258.5367 0001162 80.5035 279.6097 15.30192433 02
| Epoch (UTC): | 25 May 2026 14:00:23 |
| Eccentricity: | 0.0001162 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 258.5367° |
| argument of perigee: | 80.5035° |
| revolutions per day: | 15.30192433 |
| mean anomaly at epoch: | 279.6097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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