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 59499U 26145.35907285 +.00000000 +00000-0 +99561-4 0 00000
2 59499 42.9989 266.5417 0000832 276.4160 83.6597 15.27584300 02
| Epoch (UTC): | 25 May 2026 08:37:03 |
| Eccentricity: | 0.0000832 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.5417° |
| argument of perigee: | 276.4160° |
| revolutions per day: | 15.27584300 |
| mean anomaly at epoch: | 83.6597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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