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 59842U 26145.50705002 +.00000000 +00000-0 +14259-3 0 00002
2 59842 42.9991 200.6545 0001384 272.9743 87.0950 15.27582899 01
| Epoch (UTC): | 25 May 2026 12:10:09 |
| Eccentricity: | 0.0001384 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.6545° |
| argument of perigee: | 272.9743° |
| revolutions per day: | 15.27582899 |
| mean anomaly at epoch: | 87.0950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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