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 59010U 26145.20975078 +.00000000 +00000-0 -56059-4 0 00004
2 59010 53.1615 83.0677 0001490 97.1677 262.9493 15.30171939 04
| Epoch (UTC): | 25 May 2026 05:02:02 |
| Eccentricity: | 0.0001490 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 83.0677° |
| argument of perigee: | 97.1677° |
| revolutions per day: | 15.30171939 |
| mean anomaly at epoch: | 262.9493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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