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 59963U 26145.47987428 +.00000000 +00000-0 +75164-4 0 00009
2 59963 53.1608 68.8282 0001432 134.2591 225.8528 15.30208736 03
| Epoch (UTC): | 25 May 2026 11:31:01 |
| Eccentricity: | 0.0001432 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.8282° |
| argument of perigee: | 134.2591° |
| revolutions per day: | 15.30208736 |
| mean anomaly at epoch: | 225.8528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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