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 59703U 26144.85038161 +.00000000 +00000-0 +20623-5 0 00004
2 59703 43.0022 349.4650 0001323 268.1593 91.9107 15.27578416 04
| Epoch (UTC): | 24 May 2026 20:24:32 |
| Eccentricity: | 0.0001323 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.4650° |
| argument of perigee: | 268.1593° |
| revolutions per day: | 15.27578416 |
| mean anomaly at epoch: | 91.9107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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