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 59018U 26145.51836149 +.00000000 +00000-0 +35655-4 0 00009
2 59018 53.1608 81.4399 0001236 93.4782 266.6360 15.30196313 08
| Epoch (UTC): | 25 May 2026 12:26:26 |
| Eccentricity: | 0.0001236 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.4399° |
| argument of perigee: | 93.4782° |
| revolutions per day: | 15.30196313 |
| mean anomaly at epoch: | 266.6360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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