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 59065U 26145.52350156 +.00000000 +00000-0 +21136-3 0 00009
2 59065 97.4813 125.7401 0009210 183.7778 176.3403 15.45196753 02
| Epoch (UTC): | 25 May 2026 12:33:50 |
| Eccentricity: | 0.0009210 |
| inclination: | 97.4813° |
| perigee height: | 425 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 125.7401° |
| argument of perigee: | 183.7778° |
| revolutions per day: | 15.45196753 |
| mean anomaly at epoch: | 176.3403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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