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 59238U 26145.48485522 +.00000000 +00000-0 +10053-4 0 00009
2 59238 43.0005 69.6032 0001206 269.2044 90.8670 15.27579394 05
| Epoch (UTC): | 25 May 2026 11:38:11 |
| Eccentricity: | 0.0001206 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.6032° |
| argument of perigee: | 269.2044° |
| revolutions per day: | 15.27579394 |
| mean anomaly at epoch: | 90.8670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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