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 59400U 26145.55342317 +.00000000 +00000-0 +22419-4 0 00001
2 59400 43.0022 341.8696 0001077 271.5188 88.5541 15.27577774 08
| Epoch (UTC): | 25 May 2026 13:16:55 |
| Eccentricity: | 0.0001077 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 341.8696° |
| argument of perigee: | 271.5188° |
| revolutions per day: | 15.27577774 |
| mean anomaly at epoch: | 88.5541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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