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 59836U 26145.58656182 +.00000000 +00000-0 +15898-3 0 00007
2 59836 43.0000 200.3936 0000493 207.9532 152.1293 15.27583636 06
| Epoch (UTC): | 25 May 2026 14:04:38 |
| Eccentricity: | 0.0000493 |
| inclination: | 43.0000° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 200.3936° |
| argument of perigee: | 207.9532° |
| revolutions per day: | 15.27583636 |
| mean anomaly at epoch: | 152.1293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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