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 59467U 26145.21777449 +.00000000 +00000-0 +57892-4 0 00008
2 59467 43.0038 322.5942 0002210 271.0779 88.9819 15.27578784 03
| Epoch (UTC): | 25 May 2026 05:13:35 |
| Eccentricity: | 0.0002210 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 322.5942° |
| argument of perigee: | 271.0779° |
| revolutions per day: | 15.27578784 |
| mean anomaly at epoch: | 88.9819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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