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 59199U 26144.99887588 +.00000000 +00000-0 +11066-3 0 00002
2 59199 43.0018 21.4357 0001444 272.6872 87.3814 15.27588034 04
| Epoch (UTC): | 24 May 2026 23:58:22 |
| Eccentricity: | 0.0001444 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.4357° |
| argument of perigee: | 272.6872° |
| revolutions per day: | 15.27588034 |
| mean anomaly at epoch: | 87.3814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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